sae 2011 international conference on aircraft and engine ... · helicopter fuselage as well as the...
TRANSCRIPT
Monday, June 13
Monday, June 13
Monday, June 13
Opening Plenary Session (Part 1 of 2)
Opening Plenary Session (Part 2 of 2)
Rotorcraft Icing (Part 1of 2)
Session Code:
Session Code:
Session Code:
ICE11
ICE11
ICE5
Room Empire Ballroom
Room Empire Ballroom
Room Salon 2
This session covers testing of rotorcraft subsystems as well as modeling and analysis in support of rotorcraft in-flight icing. This session alsodescribes Computational Fluid Dynamics (CFD) codes that have been applied to rotary wing aircraft problems. The numerical simulation of icing on ahelicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady conditions are the subject of the CFD. ICE6 alsoincludes presentations related directly to rotorcraft.
Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research Center
Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research Center
Moderators -
Moderators -
9:15 a.m.
9:45 a.m.
10:15 a.m.
11:15 a.m.
11:45 a.m.
12:15 p.m.
ORAL ONLY
ORAL ONLY
ORAL ONLY
ORAL ONLY
ORAL ONLY
ORAL ONLY
Icing: Accident Driven Actions and Inactions
NASA's Research in Aviation Safety
Icing Conditions: From Research to Operation - Observation andPredictability
The Current State and Future Goals of Icing Analysis Tools and TheirImpact on Aerodynamic Design
Aircraft Development and Certification for Safe and Efficient Operationin Icing Conditions
Managing Winter Challenges at Worlds Busiest Winter Airports
Earl Weener, National Transportation Safety Board
Douglas A. Rohn, NASA John Glenn Research Center
Jean-Louis Brenguier, Meteo-France
Bernard P. Paul, Cris Bosetti, Boeing Co.
Richard Lewis, Airbus SAS
Jack Lampe, United Air Lines
Time
Time
Paper No.
Paper No.
Title
Title
SAE 2011 International Conference onAircraft and Engine Icing and Ground
DeicingTechnical Session Schedule
As of 06/19/2011 07:40 pm
9:15 a.m.
11:15 a.m.
2:30 p.m.
Session Time:
Session Time:
Session Time:
Monday, June 13
Monday, June 13
Rotorcraft Icing (Part 2 of 2)
Ice Phobic Materials (Part 1of 2)
Session Code:
Session Code:
ICE5
ICE9
Room Salon 2
Room Salon 3
This session covers testing of rotorcraft subsystems as well as modeling and analysis in support of rotorcraft in-flight icing. This session alsodescribes Computational Fluid Dynamics (CFD) codes that have been applied to rotary wing aircraft problems. The numerical simulation of icing on ahelicopter fuselage as well as the ice accretion on a hovering rotor and ice accretion in unsteady conditions are the subject of the CFD. ICE6 alsoincludes presentations related directly to rotorcraft.
This session presents both inflight and ground ice phobic ice protection research material. Included is information associated with concepts andmaterials that can prevent ice accretion or reduce the adhesion of ice.
Robert J. Flemming, Sikorsky Aircraft Corp.; Robert Leschi, Eurocopter; Richard Lewis, Airbus SAS
Philip J. Alldridge, Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Richard Moser, AerotexUK
Organizers -
Organizers -
Organizers -
Robert Leschi, Eurocopter
Philip J. Alldridge, Sikorsky Aircraft Corp.
Richard Moser, Aerotex UK
Chairpersons -
Chairpersons -
Chairpersons -
2:30 p.m.
3:00 p.m.
3:30 p.m.
4:30 p.m.
5:00 p.m.
2011-38-0006
2011-38-0014
2011-38-0008
2011-38-0015
2011-38-0016
Certification of the Sikorsky S-92A¿ Helicopter to the EASA LimitedIcing Special Condition
Extrapolation of Wind Tunnel Ice Shapes in the Evaluation of the Needfor Horizontal Tail Ice Protection on the BA609 Tiltrotor
The Certification of Externally-mounted Components on HelicoptersCertificated for Flight in Icing Conditions
Calculations of Ice Shapes on Oscillating Airfoils
Oscillating Airfoil Icing Tests in the NASA Glenn Research Center IcingResearch Tunnel
Robert J. Flemming, Sikorsky Aircraft Corp.; Philip Alldridge, SikorskyAircraft Corp
Jason Wright, Roger J. Aubert, Bell Helicopter Textron
Philip J. Alldridge, Robert J. Flemming, Sikorsky Aircraft Corp.
Robert Narducci, Tonja Reinert, The Boeing Company
Tonja Reinert, Boeing Co.; Robert J. Flemming, Sikorsky Aircraft Corp.;Robert Narducci, Boeing Co.; Roger J. Aubert, Bell Helicopter Textron
ORAL ONLY
Time
Time
Time
Paper No.
Paper No.
Paper No.
Title
Title
Title
4:30 p.m.
2:30 p.m.
Session Time:
Session Time:
Monday, June 13
Monday, June 13
Ice Phobic Materials (Part 2 of 2)
CFD Icing Simulation Tools (Part 1of 6)
Session Code:
Session Code:
ICE9
ICE1
Room Salon 3
Room Salon 6
This session presents both inflight and ground ice phobic ice protection research material. Included is information associated with concepts andmaterials that can prevent ice accretion or reduce the adhesion of ice.
This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Lakshmi N. Sankar,Georgia Institute of Technology
Organizers -
Organizers -
Richard Lewis, Airbus SAS
Lakshmi N. Sankar, Georgia Institute of Technology
Chairpersons -
Chairpersons -
2:30 p.m.
3:00 p.m.
3:30 p.m.
4:30 p.m.
5:00 p.m.
2:30 p.m.
2011-38-0001
2011-38-0002
2011-38-0003
2011-38-0009
2011-38-0010
2011-38-0106
In-Silico Environment for Designing Anti-icing Surfaces
Ice Phobic Coatings on Controlled and Covered Surfaces
Experimental Study of Hybrid Anti-Icing Systems CombiningThermoelectric and Hydrophobic Coatings
Surface Coating Effect on Protection of Icing for Axial Fan Blade
Hydrophobic Coating Study for Anti-icing Aircraft
Parallel Computing Applied to Three-Dimensional Droplet TrajectorySimulation in Lagrangian Approach
Jie Xiao, Katherine E. Mackie, Washington State Univ.; Joseph H. Osborne,Jill Seebergh, Boeing Research & Technology; Santanu Chaudhuri,Washington State Univ.
Brian Burkitt, Nathan Lipps, Nusil Technology
Guy Fortin, Maryelle Adomou, Jean Perron, Univ. du Quebec a Chicoutimi
Takeshi Murooka, Shinichirou Shishido, IHI Corp.; Riho Hiramoto, TakakazuMinoya, Hokkaido Institute of Technology
Katsuaki Morita, Koji Okamoto, Univ. of Tokyo; Akihito Aoki, Shigeo Kimura,Kanagawa Institute of Technology; Hirotaka Sakaue, Japan AerospaceExploration Agency
Ozgen Serkan, Middle East Technical University; Tarhan Erhan, CanibekMurat, Turkish Aerospace Industries Inc.
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
4:30 p.m.
2:30 p.m.
Session Time:
Session Time:
Monday, June 13
Tuesday, June 14
CFD Icing Simulation Tools (Part 2 of 6)
Appendix D: Ice Crystal Icing (Part 1of 4)
Session Code:
Session Code:
ICE1
ICE4
Room Salon 6
Room Salon 2
This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.
This session deals with every aspect of flight in what is now known as Appendix D icing conditions, flight in clouds with ice crystal content. Thesession includes papers that present planning for future ice crystal research, the development of ice crystal test facilities, and wind tunnel and flighttests to gather ice crystal data and data on the effects of ice crystals. Since ice crystals generally affect only turbine engines, this session will have astrong emphasis on engine icing.
Robert J. Flemming, Sikorsky Aircraft Corp.; Daniel C. Knezevici, National Research CouncilCanada; Richard Lewis, Airbus SAS
Tom Currie, National Research Council Canada; Robert J. Flemming, Sikorsky Aircraft Corp.;Richard Lewis, Airbus SAS
Organizers -
Organizers -
Daniel C. Knezevici, National Research Council Canada
Tom Currie, National Research Council Canada
Chairpersons -
Chairpersons -
3:00 p.m.
3:30 p.m.
4:30 p.m.
5:00 p.m.
8:30 a.m.
9:00 a.m.
2011-38-0004
2011-38-0005
2011-38-0011
2011-38-0013
2011-38-0017
2011-38-0079
Improvements in Numerical Analysis of Droplet Impingement UsingLagrangian Approach
Lagrangian Parcel Volume Method for Unsteady Particle Concentration
Aircraft Icing and Anti-Icing Simulation Code CANICE3D: Panel Methodvs. CFD
Impingement of Supercooled Large Droplets via Reduced Order Models
An Overview of NASA Engine Ice-Crystal Icing Research
Development and Commissioning of a Linear Compressor Cascade Rigfor Ice Crystal Research
Peng Ke, Xinxin Wang, Beihang University
Jason Mickey, Eric Loth, Univ. of Virginia; Colin Bidwell, NASA
Jaideep Galhawat, Ion Paraschivoiu, Ecole Polytechnique Montreal; FarooqSaeed, King Fahd Univ. of Petroleum & Minerals
Marco Fossati, Wagdi G. Habashi, McGill University; Guido Baruzzi,Newmerical Technologies Inc.
Harold E. Addy, Jr., Joseph P. Veres, NASA Glenn Research Center
Daniel C. Knezevici, Dan Fuleki, James MacLeod, National ResearchCouncil Canada
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
4:30 p.m.
8:30 a.m.
Session Time:
Session Time:
Tuesday, June 14
Tuesday, June 14
Appendix D: Ice Crystal Icing (Part 2 of 4)
Appendix D: Ice Crystal Icing (Part 3 of 4)
Session Code:
Session Code:
ICE4
ICE4
Room Salon 2
Room Salon 2
This session deals with every aspect of flight in what is now known as Appendix D icing conditions, flight in clouds with ice crystal content. Thesession includes papers that present planning for future ice crystal research, the development of ice crystal test facilities, and wind tunnel and flighttests to gather ice crystal data and data on the effects of ice crystals. Since ice crystals generally affect only turbine engines, this session will have astrong emphasis on engine icing.
This session deals with every aspect of flight in what is now known as Appendix D icing conditions, flight in clouds with ice crystal content. Thesession includes papers that present planning for future ice crystal research, the development of ice crystal test facilities, and wind tunnel and flighttests to gather ice crystal data and data on the effects of ice crystals. Since ice crystals generally affect only turbine engines, this session will have astrong emphasis on engine icing.
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Jen-Ching Tsao, OhioAerospace Institute
Philip Chow; Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS
Organizers -
Organizers -
Jen-Ching Tsao, Ohio Aerospace Institute
Philip Chow
Chairpersons -
Chairpersons -
9:30 a.m.
10:30 a.m.
11:00 a.m.
11:30 a.m.
2011-38-0018
2011-38-0025
2011-38-0026
2011-38-0027
Fundamental Ice Crystal Accretion Physics Studies
Engine Icing Modeling and Simulation (Part I): Ice Crystal Accretion onCompression System Components and Modeling its Effects on EnginePerformance
Engine Icing Modeling and Simulation (Part 2): Performance Simulationof Engine Rollback Phenomena
Atmosphere Sampling: Airbus A340 Flight Tests in Glaciated IcingConditions
Peter Struk, NASA John Glenn Research Center; Tom Currie, NationalResearch Council Canada; William Benjamin Wright, ASRC Aerospace;Daniel C. Knezevici, Dan Fuleki, National Research Council Canada; AndyBroeren, Mario Vargas, NASA; Jen-Ching Tsao, Ohio Aerospace Institute
Philip C. E. Jorgenson, NASA; Jospeh P. Veres, NASA John GlennResearch Center; William B. Wright, Ryan D. May, ASRC Aerospace
Ryan D. May, ASRC Aerospace; Ten-Huei Guo, Joseph P. Veres, Philip C.E. Jorgenson, NASA John Glenn Research Center
Alice Grandin, Airbus Operations S.A.S.ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
10:30 a.m.
1:30 p.m.
Session Time:
Session Time:
Tuesday, June 14
Tuesday, June 14
Appendix D: Ice Crystal Icing (Part 4 of 4)
Meteorological Studies of Icing Conditions (Part 1 of 2)
Session Code:
Session Code:
ICE4
ICE17
Room Salon 2
Room Salon 3
Due to aircraft power budget limitations, there is a constant effort to minimize the energy requirements of ice protection systems. Numerical tools canbe used to optimize such systems but there is very little data available to validate the tools. This session will present details of ice protection systemsand their validation.
This session will focus on observational studies of in-flight icing events, the characterization of icing environments and ways to communicate that information to users.
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Jeanne G. Mason, BoeingCommercial Airplanes
Ben C. Bernstein, Leading Edge Atmospherics; George A. Isaac, Environment Canada; ChristineLeBot, Meteo-France
Organizers -
Organizers -
Jeanne G. Mason, Boeing Commercial Airplanes
George A. Isaac, Environment Canada
Chairpersons -
Chairpersons -
1:30 p.m.
2:00 p.m.
2:30 p.m.
3:30 p.m.
4:00 p.m.
4:30 p.m.
2011-38-0036
2011-38-0037
2011-38-0038
2011-38-0048
2011-38-0049
2011-38-0050
Naturally Aspirating Isokinetic Total Water Content Probe: Wind TunnelTest Results and Design Modifications
Modifications at the Glenn Research Center's Propulsion SystemsLaboratory to Evaluate High Altitude Engine Icing Phenomena
Altitude Icing Testing of Jet Engines to begin at NASA Glenn ResearchCenter Propulsion Systems Laboratory
Particle Trajectory and Icing Analysis of the E<sup>3</sup> TurbofanEngine Using LEWICE3D Version 3
Critical Point Evaluation of Ice Crystals in Turbofan Engines
An Analysis of Turbofan Inlet Water and Ice Concentration Effects inIcing Conditions
Craig Davison, National Research Council Canada; Thomas Ratvasky,NASA John Glenn Research Center; Lyle Lilie, Science EngineeringAssociates
George Sydnor, NASA Langley Research Center; Jeffrey A. Chambers,NASA John Glenn Research Center
Thomas Hoffman, Paul Lizanich, Thomas Griffin, NASA John GlennResearch Center
Colin Bidwell, NASA
Robert S. Mazzawy, Trebor Systems Inc.
Shengfang Liao, Xuejun Liu, Matthew Feulner, United Technologies Prattand Whitney
ORAL ONLY
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
3:30 p.m.
8:30 a.m.
Session Time:
Session Time:
Tuesday, June 14
Tuesday, June 14
Remote Sensing of Atmospheric Icing Conditions (Part 1 of 2)
Remote Sensing of Atmospheric Icing Conditions (Part 2 of 2)
Session Code:
Session Code:
ICE18
ICE18
Room Salon 3
Room Salon 3
This session will focus on methods used to diagnose the presence of icing conditions using remote sensing using ground-based systems.
This session will focus on methods used to diagnose the presence of icing conditions using remote sensing using satellite-based and in-flightsystems.
Ben C. Bernstein, Leading Edge Atmospherics; Christine LeBot, Meteo-France; Cory Wolff,National Center for Atmospheric Research
Ben C. Bernstein, Leading Edge Atmospherics; Julie Haggerty, NCAR; Christine LeBot, Meteo-France
Organizers -
Organizers -
Cory Wolff, National Center for Atmospheric Research
Julie Haggerty, NCAR
Chairpersons -
Chairpersons -
8:30 a.m.
9:00 a.m.
9:30 a.m.
10:30 a.m.
11:00 a.m.
11:30 a.m.
2011-38-0019
2011-38-0020
2011-38-0021
2011-38-0028
2011-38-0029
2011-38-0030
Initial Steps Toward Inclusion of Icing-Relevant AtmosphericParameters in a Weather Forecast
An Examination of Aircraft Icing Conditions Associated with Cold Fronts
A Regional Comparison of Icing Conditions in Boundary Layer Clouds
A Freezing Fog/Drizzle Event during the FRAM-S Project
Decision Making Regarding Aircraft De-Icing and In-Flight Icing Usingthe Canadian Airport Nowcasting System (CAN-Now)
In-flight Icing Hazard Verification with NASA's Icing Remote SensingSystem for Development of a NEXRAD Icing Hazard Level Algorithm
Marcia K. Politovich, Daniel R. Adriaansen, Gregory Thompson, NationalCenter for Atmospheric Research
Cory Wolff, Frank Mcdonough, National Center for Atmospheric Research;Ben Bernstein, Leading Edge Atmospherics
Ben C. Bernstein, Leading Edge Atmospherics; Frank Mcdonough, CoryWolff, National Center for Atmospheric Research
Ismail Gultepe, Meteorological Service of Canada; George A. Isaac,Environment Canada; Roy Martin Rasmussen, National Center forAtmospheric Research; K. Ungar, Health Canada
George A. Isaac, Monika Bailey, Faisal Boudala, Stewart G. Cober, RobertCrawford, Norman Donaldson, Ismail Gultepe, Bjarne Hansen, IvanHeckman, Laura Huang, Alister Ling, Janti Reid, ARMP, EnvironmentCanada; Marc Fournier, CMAC-E, Environment Canada
David Serke, NCAR/RAL; John Hubbert, NCAR/EOL; Andrew Reehorst,NASA Glenn Research Center; Marcia Politovich, NCAR/RAL; PatrickKennedy, Colorado State University; Mike Dixon, Scott Ellis, NCAR/EOL;Chris Johnston, David Albo, Scott Landolt, NCAR/RAL
ORAL ONLY
Time Paper No. Title
10:30 a.m.
1:30 p.m.
Session Time:
Session Time:
Tuesday, June 14
Tuesday, June 14
Meteorological Studies of Icing Conditions (Part 2 of 2)
CFD Icing Simulation Tools (Part 3 of 6)
Session Code:
Session Code:
ICE17
ICE1
Room Salon 3
Room Salon 6
This session will focus on observational studies of in-flight icing events, the characterization of icing environments and ways to communicate thatinformation to users. Mixed-phase icing environments are highlighted here.
This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.
Ben C. Bernstein, Leading Edge Atmospherics; Christine LeBot, Meteo-France; Jakob Tendel,Leibniz University Hannover
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; William B. Wright, ASRCAerospace
Organizers -
Organizers -
Jakob Tendel, Leibniz University Hannover
William B. Wright, ASRC Aerospace
Chairpersons -
Chairpersons -
1:30 p.m.
2:00 p.m.
2:30 p.m.
3:30 p.m.
4:00 p.m.
4:30 p.m.
2011-38-0039
2011-38-0040
2011-38-0041
2011-38-0051
2011-38-0052
2011-38-0053
Characterization of Aircraft Icing Environment using Airborne Radarsand Radiometer
New Methods to Infer Aircraft Icing Conditions using Satellite Data
Nowcasting Aircraft Icing Conditions in the Presence of MultilayeredClouds Using Meteorological Satellite Data
Using the TAMDAR Sensor for In-flight Ice Detection and ImprovedSafety of Flight
The Large and Small-Scale Structure and Evolution of a Mixed-PhaseIcing Cloud
Aircraft Icing Under an Evolving Mixed Phase Environment
Mengistu Wolde, Institute for Aerospace Studies
William Smith, Patrick Minnis, NASA Langley Research Center; CeciliaFleeger, Douglas Spangenberg, Science Systems & Applications Inc.; DavidSerke, NCAR; Andrew Reehorst, NASA John Glenn Research Center
Douglas Spangenberg, Science Systems & Applications Inc.; Patrick Minnis,William Smith, NASA Langley Research Center; Fu-Lung Chang, ScienceSystems & Applications Inc
Jamie Braid, Patrick Van Wie, Jeffrey Rex, AirDat LLC
Frank Mcdonough, Cory Wolff, National Center for Atmospheric Research
John Hallett, Desert Research Institute
ORAL ONLY
ORAL ONLY
ORAL ONLY
Time
Time
Time
Paper No.
Paper No.
Paper No.
Title
Title
Title
3:30 p.m.
8:30 a.m.
Session Time:
Session Time:
Tuesday, June 14
Tuesday, June 14
CFD Icing Simulation Tools (Part 4 of 6)
CFD Icing Simulation Tools (Part 5 of 6)
Session Code:
Session Code:
ICE1
ICE1
Room Salon 6
Room Salon 6
This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.
This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Robert Narducci, TheBoeing Company
Robert J. Flemming, Sikorsky Aircraft Corp.; Wagdi G. Habashi, McGill Univ.; Richard Lewis, AirbusSAS
Organizers -
Organizers -
Robert Narducci, Boeing Helicopters
Wagdi G. Habashi, McGill Univ.
Chairpersons -
Chairpersons -
8:30 a.m.
9:00 a.m.
9:30 a.m.
10:30 a.m.
11:00 a.m.
11:30 a.m.
2011-38-0022
2011-38-0023
2011-38-0024
2011-38-0031
2011-38-0032
2011-38-0033
Robust Moving Meshes for the Prediction of Aerodynamic Degradationduring In-Flight Icing
Proposed Wall Function Models for Heat Transfer around a Cylinder withRough Surface in Cross Flow
FENSAP-ICE: Numerical Prediction of Ice Roughness Evolution, and itsEffects on Ice Shapes
CFD-Icing: A Predictive Tool for In-Flight Icing Risk Management
Efficient Prediction of Ice Shapes in CFD Simulation of In-flight IcingUsing a POD-Based Reduced Order Model
FENSAP-ICE in Aid of Certification: From CFD to Flight Testing
Marco Fossati, Rooh-ul-Amin Khurram, Wagdi G. Habashi, McGill Univ.
Guilherme Araujo Lima da Silva, Marcos Noboru Arima, Aero-ThermalSolutions for Industry; Natashe Nicoli Branco, Marcos de Mattos Pimenta,University of São Paulo
Isik A. Ozcer, Guido S. Baruzzi, Thomas Reid, Newmerical TechnologiesInc.; Wagdi G. Habashi, Marco Fossati, McGill Univ.; Giulio Croce,Universita degli Studi di Udine
Danial Zeppetelli, Wagdi G. Habashi, McGill Univ.
Sung Ki Jung, Gyeongsang National Univ.; Rho Shin Myong, Tae HwanCho, GNU, Dept. of Aero. Sys. Eng. and ReCAPT
John P. Dow, Sr., DOW International, L.L.C.; Cristhian N. Aliaga, ShoaibShah, Jian Chen, Newmerical Technologies Inc.; Wagdi G. Habashi, McGillUniv.; John L. Siemens, JLS Eningeering Consultants Inc.
Time Paper No. Title
10:30 a.m.
1:30 p.m.
Session Time:
Session Time:
Tuesday, June 14
Wednesday, June 15
CFD Icing Simulation Tools (Part 6 of 6)
The Effects of Icing (Part 1of 2)
Session Code:
Session Code:
ICE1
ICE2
Room Salon 6
Room Salon 2
This session, comprised of six parts, provides information on developments in the use of CFD to simulate all facets of inflight icing, including droptrajectories, impingement, and accretion. Particular emphasis is on methods for physical modeling, for increased geometric complexity, for processintegration, and in the validation of the methodology.
This session includes material on the effects of icing and ice accretion on the performance and flying characteristics of aircraft and on methods anddata used to support certification to 14 CFR 25 Part B (or the equivalent for other aircraft types and regulatory standards).
Michael B. Bragg, Univ. of Illinois at Urbana-Champaign; Robert J. Flemming, Sikorsky AircraftCorp.; Richard Lewis, Airbus SAS
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS
Organizers -
Organizers -
Michael B. Bragg, Univ. of Illinois at Urbana-Champaign
Robert J. Flemming, Sikorsky Aircraft Corp.
Chairpersons -
Chairpersons -
1:30 p.m.
2:00 p.m.
2:30 p.m.
3:30 p.m.
4:00 p.m.
4:30 p.m.
2011-38-0054
2011-38-0043
2011-38-0044
2011-38-0055
2011-38-0056
ORAL ONLY
Improving Ice Accretion Simulation Through the use of CFD
Simulation of Ice Accretion on Three Dimensional Wing
A CFD Approach for Predicting 3D Ice Accretion on Aircraft
Analysis for the Design and Test of an Ice Protection System for aScoop Intake
Development of An Icing Tool For Aircraft Engines
Propulsion Icing Wind Tunnel Research Simulating Ice Pellet Conditions
Daniel Martins Silva, Instituto Tecnológico de Aeronaútica-ITA; LuisGustavo Trapp, Embraer Aircraft Corp.
Chao Wang, Shi-nan Chang, Beijing Univ. Aeronautics & Astronautics; Xin-ming Su, China Academy of Space Technology
Michael P. Kinzel, Ralph W. Noack, Christian M. Sarofeen, David Boger,Penn State Univ.-Applied Research Lab.; Richard Eric Kreeger, NASA JohnGlenn Research Center
Richard Moser, Roger Gent, Aerotex UK
Chiong S. Tan, GE Global Research Center; Byron Pritchard, Ron Plybon,Chuck Califf, Ray Holm, Sasikumar Muthusamy, Viilas Bokade, TS Niranjan,Balasubramaniam Mahadevan, General Electric Co
Marco Ruggi, APS Aviation Inc.
Time
Time
Time
Paper No.
Paper No.
Paper No.
Title
Title
Title
3:30 p.m.
8:30 a.m.
Session Time:
Session Time:
Wednesday, June 15
Wednesday, June 15
The Effects of Icing (Part 2 of 2)
Ice Shedding and Ice Scaling (Part 1of 2)
Session Code:
Session Code:
ICE2
ICE6
Room Salon 2
Room Salon 2
This session includes material on the effects of icing and ice accretion on the performance and flying characteristics of aircraft and on methods anddata used to support certification to 14 CFR 25 Part B (or the equivalent for other aircraft types and regulatory standards).
This session includes papers dedicated to the shedding of ice from aircraft components as well as scaling relationships to allow the application tomodel-scale data to full-scale problems.
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Tonja Reinert, Boeing Co.
Roger J. Aubert, Bell Helicopter Textron; Robert J. Flemming, Sikorsky Aircraft Corp.; RichardLewis, Airbus SAS
Organizers -
Organizers -
Tonja Reinert, Boeing Co.
Roger J. Aubert, Bell Helicopter Textron
Chairpersons -
Chairpersons -
8:30 a.m.
9:00 a.m.
9:30 a.m.
10:30 a.m.
11:00 a.m.
1:30 p.m.
2:00 p.m.
2011-38-0065
2011-38-0066
2011-38-0067
2011-38-0073
2011-38-0074
2011-38-0081
2011-38-0082
Aerodynamic Effects of Simulated Ice Accretion on a Generic TransportModel
Envelope Protection System for Iced Airfoils Using Flap Hinge Moment
Low Speed Aerodynamic Study of Full-Scale Figh-Fidelity Runback IceShapes
Aircraft Performance Degradation - the Effects of Inflight Icing upon Lift,Drag and Propulsive Efficiency
Flow Field Predictions of the NASA Glenn Icing Research Tunnel
Evaluation of Icing Scaling on Swept NACA 0012 Airfoil Models
Icing Scaling Laws Implemented in a Rotor Performance DegradationModel
Andy P. Broeren, NASA Glenn Research Center; Sam Lee, ASRCAerospace Corporation; Gautam H. Shah, Patrick C. Murphy, NASA LangleyResearch Center
Phillip J. Ansell, Michael B. Bragg, Univ. of Illinois at Urbana-Champaign;Michael F. Kerho, Rolling Hills Research Corp.
Nathalie Alegre, David Hammond, Cranfield Univ.
Anthony P. Brown, National Research Council Canada
Kevin M. Clark, Yong Han Yeong, Eric Loth, Univ. of Virginia; Judith FossVan Zante, David Sheldon, Robert Ide, NASA John Glenn Research Center
Jen-Ching Tsao, Ohio Aerospace Institute; Sam Lee, ASRC AerospaceCorp.
Stephane Catris, Eurocopter
Time
Time
Paper No.
Paper No.
Title
Title
ALL DAY
1:30 p.m.
Session Time:
Session Time:
Wednesday, June 15
Wednesday, June 15
Wednesday, June 15
Ice Shedding and Ice Scaling (Part 2 of 2)
Applications of Weather Models for In-Flight Icing Diagnosis and Forecasting
Real-time Icing Products
Session Code:
Session Code:
Session Code:
ICE6
ICE23
ICE22
Room Salon 2
Room Salon 3
This session includes papers dedicated to the shedding of ice from aircraft components as well as scaling relationships to allow the application tomodel-scale data to full-scale problems.
This session will focus on the advancement of cloud microphysics schemes used to explicitly predict supercooled liquid water content and drop size,as well as their application in real-time icing systems.
Robert J. Flemming, Sikorsky Aircraft Corp.; Roger Gent, Aerotex UK; Richard Lewis, Airbus SAS
Ben C. Bernstein, Leading Edge Atmospherics; Gordon Brooks, Air Force Weather Agency;Christine LeBot, Meteo-France
Organizers -
Organizers -
Roger Gent, Aer
Gordon Brooks, Air Force Weather Agency
Chairpersons -
Chairpersons -
2:30 p.m.
3:30 p.m.
4:00 p.m.
8:30 a.m.
9:00 a.m.
2011-38-0083
2011-38-0089
2011-38-0090
2011-38-0060
2011-38-0062
Further Evaluation of Scaling Methods for Rotorcraft Icing
FENSAP-ICE: A CFD Monte Carlo Approach to Shed-Ice Trajectory andImpact
A Methodology for the Prediction of Rotor Blade Ice Formation andShedding
Applications of an Advanced Cloud and Precipitation Physics Packagein a Weather Forecast Model
Microphysics from High Resolution NWP Model in the IcingIdentification Tool Sigma
Jen-Ching Tsao, Ohio Aerospace Institute; Richard Kreeger, NASA JohnGlenn Research Center
Jean-Mathieu Deschenes, McGill Univ.; Guido S. Baruzzi, Patrick Lagace,Newmerical Technologies Inc.; Wagdi G. Habashi, McGill Univ.
Jeremy Bain, Lakshmi N. Sankar, Georgia Institute of Technology; Roger J.Aubert, Bell Helicopter Textron; Robert J. Flemming, Sikorsky Aircraft Corp.
Gregory Thompson, Changhai Liu, Marcia Politovich, National Center forAtmospheric Research
Christine LeBot, Meteo-France
ORAL ONLY
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
3:30 p.m.
8:30 a.m.
Session Time:
Session Time:
Wednesday, June 15
Wednesday, June 15
High Ice-water Content and Jet Engine Icing
Aircraft Anti-icing and Deicing Operations (Part 1of 4)
Session Code:
Session Code:
ICE21
ICE10
Room Salon 3
Room Salon 3
Room Salon 3
This session will focus on real-time icing products that merge information from a variety of sources, with emphasis on their performance, strengthsand weaknesses and their adaptation to new environments.
This session will focus on the phenomenon of jet engine icing associated with the presence of large concentrations of ice crystals. Examinations ofrecent events, planned field program work and new techniques to detect these events will be discussed.
Ben C. Bernstein, Leading Edge Atmospherics; Christine LeBot, Meteo-France
Ben C. Bernstein, Leading Edge Atmospherics; Jonathan Gould, Pratt & Whitney; Christine LeBot,Meteo-France
Organizers -
Organizers -
Ben C. Bernstein, Leading Edge Atmospherics; Christine LeBot, Meteo-France
Jonathan Gould, Pratt & Whitney
Chairpersons -
Chairpersons -
10:30 a.m.
11:00 a.m.
11:30 a.m.
1:30 p.m.
2:00 p.m.
2:30 p.m.
2011-38-0068
2011-38-0069
2011-38-0070
ORAL ONLY
2011-38-0094
2011-38-0095
Verification of ADWICE In-Flight Icing Forecasts: Performance vsPIREPS Compared to FIP
Exercising CIP Severity: An Investigation of Methodologies within theCIP Severity Algorithm
LOWICE: An Example of the Adaption of In-flight Icing DiagnosisConcepts to the Structural Icing Environment
High Ice Water Content Cloud Characterization Flight Campaign Update
The Challenges Identifying Weather Associated With Jet Engine IceCrystal Icing
Preliminary Algorithm for High Ice Water Content Detection
Jakob Tendel, Leibniz Universität Hannover; Cory Wolff, National Center forAtmospheric Research
Daniel R. Adriaansen, Cory Wolff, Frank Mcdonough, National Center forAtmospheric Research
Ben C. Bernstein, Leading Edge Atmospherics; Erik Gregow, FinnishMeteorological Institute; Ian Wittmeyer, Leading Edge Atmospherics; JarkkoHirvonen, Finnish Meteorological Institute
Thomas Ratvasky, NASA John Glenn Research Center; J. Walter Strapp,Environment Canada
Jeanne G. Mason, Matthew Grzych, Boeing Commercial Airplanes
Jennifer Black, Julie Haggerty, NCAR; Frank Mcdonough, Marcia K.Politovich, National Center for Atmospheric Research
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
10:30 a.m.
1:30 p.m.
3:30 p.m.
Session Time:
Session Time:
Session Time:
Wednesday, June 15
Wednesday, June 15
Appendix O: SLD Icing (Part 1 of 4)
Appendix O: SLD Icing (Part 2 of 4)
Session Code:
Session Code:
ICE3
ICE3
Room Salon 6
Room Salon 6
This session addresses a wide variety of research topics related to aircraft ground deicing operations including active frost detection systems, liquidwater equivalent based systems to determine and update anti-icing fluid holdover times. Aircraft flight testing and wind tunnel testing with anti-icingfluids, along with fluid failure modeling, runway deicing fluid development and environmental regulations will also be discussed.
This session presents the latest developments and applications for certification to 14 CFR 25 Appendix O supercooled large drop (SLD) icingconditions. Included are topics of droplet splashing, rebound and re-impingement, and the effect they have on the resultant ice shapes.
Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration
Robert J. Flemming, Sikorsky Aircraft Corp.; Eugene G. Hill; Richard Lewis, Airbus SAS
Organizers -
Organizers -
Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration
Eugene G. Hill
Chairpersons -
Chairpersons -
3:30 p.m.
4:00 p.m.
4:30 p.m.
8:30 a.m.
9:00 a.m.
9:30 a.m.
2011-38-0045
2011-38-0046
2011-38-0047
ORAL ONLY
2011-38-0063
2011-38-0064
Experimental Study of Snow Precipitation Over a Generic Deicing Fluidwithout Fluid Flow
Using Manual Snow Pan Measurements to Verify a Liquid EquivalentWater-based System for Ground De-icing Operations
A New Technique for Automated Frost Detection
Aerodynamics Degradations and Control Anomalies during a Departurefrom Controlled Flight of a Turboprop Airplane in an SLD Environment
EXTICE: EXTreme Icing Environement
Experimental Investigation of Thin Water Film Stability and ItsCharacteristics in SLD Icing Problem
Guy Fortin, Ilham Enneji, Arlene Beisswenger, Jean Perron, Univ. duQuebec a Chicoutimi
Jennifer Black, Scott Landolt, Roy Martin Rasmussen, National Center forAtmospheric Research
Scott Landolt, Roy Martin Rasmussen, Chris Johnston, National Center forAtmospheric Research
Daniel R. Bower, Ph.D., Dennis A. Crider, National Transportation SafetyBoard
Giuseppe Mingione, Emiliano Iuliano, CIRA; Didier Guffond, ONERA;Cameron Tropea, Technical Univ. of Darmstadt
Jafar Alzaili, David Hammond, Cranfield University
ORAL ONLY
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
8:30 a.m.
10:30 a.m.
Session Time:
Session Time:
Wednesday, June 15
Wednesday, June 15
Appendix O: SLD Icing (Part 3 of 4)
Appendix O: SLD Icing (Part 4 of 4)
Session Code:
Session Code:
ICE3
ICE3
Room Salon 6
Room Salon 6
This session presents the latest developments and applications for certification to 14 CFR 25 Appendix O supercooled large drop (SLD) icingconditions. Included are topics of droplet splashing, rebound and re-impingement, and the effect they have on the resultant ice shapes.
This session presents the latest developments and applications for certification to 14 CFR 25 Appendix O supercooled large drop (SLD) icingconditions. Included are topics of droplet splashing, rebound and re-impingement, and the effect they have on the resultant ice shapes.
This session presents the latest developments and applications for certification to 14 CFR 25 Appendix O supercooled large drop (SLD) icingconditions. Included are topics of droplet splashing, rebound and re-impingement, and the effect they have on the resultant ice shapes.
Robert J. Flemming, Sikorsky Aircraft Corp.; Dan Fuleki, National Research Council Canada;Richard Lewis, Airbus SAS
Robert J. Flemming, Sikorsky Aircraft Corp.; Jim R. Hoppins, Cessna Aircraft Co.; Richard Lewis,Airbus SAS
Biagio Esposito, CIRA; Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS
Organizers -
Organizers -
Organizers -
Dan Fuleki, National Research Council Canada
Jim R. Hoppins, Cessna Aircraft Co.
Biagio Esposito, CIRA
Chairpersons -
Chairpersons -
Chairpersons -
10:30 a.m.
11:00 a.m.
11:30 a.m.
1:30 p.m.
2:00 p.m.
2:30 p.m.
ORAL ONLY
2011-38-0071
2011-38-0072
ORAL ONLY
2011-38-0080
2011-38-0086
Practical Scaling of Available IWT Conditions to the Appendix O Spectra
Numerical Simulation of SLD Ice Accretions
Wind Tunnel Investigation on the Response Characteristics of ParticleSpectrometers to SLD Cloud Conditions
Determining the Suitability of IWT Test Facilities for DemonstratingCompliance with Certification Requirements in Appendix O Conditions
CFD Analysis of Supercooled Large Droplets in Turbofan Engines
New SLD Icing Capabilities at DGA Aero-engine Testing
David C. Parkins, American Kestrel Company
Jacco Hospers, H. W. M. Hoeijmakers, Univ. of Twente
Biagio Esposito, CIRA; J. Walter Strapp, Environment Canada; William D.Bachalo, Artium Technologies Inc.; Myron Oleskiw, National ResearchCouncil Canada
Kamel Al-Khalil, Joseph Vogel, Cox & Company Inc.; David C. Parkins,American Kestrel Company
Chuck Califf, Anabel Rodriguez, Eduardo Lemini, GE Aviation; Chiong Tan,GE Global Research Center
Franck Hervy, DGA Essais Propulseurs
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
1:30 p.m.
3:30 p.m.
Session Time:
Session Time:
Thursday, June 16
Thursday, June 16
Icing Certification Plenary Session
Ice Protection Systems (Part 1 of 3)
Session Code:
Session Code:
ICE12
ICE8
Room Empire Ballroom
Room Salon 2
Due to aircraft power budget limitations, there is a constant effort to minimize the energy requirements of ice protection systems. Numerical tools canbe used to optimize such systems but there is little data available to validate the tools. This session will present details of ice protection systems andtheir validation.
Stephane Catris, Eurocopter; Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, AirbusSAS
Organizers -
Stephane Catris, EurocopterChairpersons -
Thomas H. Bond, Federal Aviation AdminstrationModerators -
3:30 p.m.
4:00 p.m.
3:30 p.m.
8:30 a.m.
9:00 a.m.
9:30 a.m.
2011-38-0087
2011-38-0088
ORAL ONLY
ORAL ONLY
2011-38-0035
2011-38-0034
Rotating Rig Development for Droplet Deformation/Breakup and ImpactInduced by Aerodynamic Surfaces
ONICE2D and DROP3D SLD Capability Assessment
Aircraft Turbine Engine Icing: Current Issues and Future Vision
Clean Sky European JTI, Systems for Green Operations - Electrical IceProtection Systems
The Building Blocks for a Hybrid ElectroThermal-ElectroMechanicalSimulation Tool
Experimental and Computer Model Results for a Bleed Air Ice ProtectionSystem
Alejandro Feo, Instituto Nacional de Técnica Aeroespacial (INTA); MarioVargas, NASA Glenn Research Center; Suthyvann Sor, Instituto Nacional deTécnica Aeroespacial (INTA)
Fabien Dezitter, Airbus
John Fisher, Federal Aviation Administration
Francois LaRue, Zodiac Aerospace
Colin Hatch, Richard Moser, Roger Gent, Aerotex UK; Peter Hicks,University College London UK
Michael Papadakis, Alonso O. Zamora Rodriguez, Rodrigo HoffmannDomingos, Wichita State Univ.
Time
Time
Time
Paper No.
Paper No.
Paper No.
Title
Title
Title
3:30 p.m.
8:30 a.m.
Session Time:
Session Time:
Thursday, June 16
Thursday, June 16
Ice Protection Systems (Part 2 of 3)
Ice Protection Systems (Part 3 of 3)
Session Code:
Session Code:
ICE8
ICE8
Room Salon 2
Room Salon 2
Due to aircraft power budget limitations, there is a constant effort to minimize the energy requirements of ice protection systems. Numerical tools canbe used to optimize such systems but there is little data available to validate the tools. This session will present details of ice protection systems andtheir validation.
Due to aircraft power budget limitations, there is a constant effort to minimize the energy requirements of ice protection systems. Numerical tools canbe used to optimize such systems but there is little data available to validate the tools. This session will present details of ice protection systems andtheir validation.
Thomas H. Bond, Federal Aviation Adminstration; Robert J. Flemming, Sikorsky Aircraft Corp.;Richard Lewis, Airbus SAS
Gene Addy, NASA John Glenn Research Center; Robert J. Flemming, Sikorsky Aircraft Corp.;Richard Lewis, Airbus SAS
Organizers -
Organizers -
Thomas H. Bond, Federal Aviation Adminstration
Gene Addy, NASA John Glenn Research Center
Chairpersons -
Chairpersons -
10:30 a.m.
11:00 a.m.
11:30 a.m.
1:30 p.m.
2:00 p.m.
2:30 p.m.
2011-38-0096
2011-38-0097
2011-38-0098
2011-38-0102
2011-38-0103
2011-38-0104
Numerical Simulation of Electro-thermal Deicing Process and theEffects of Icing Conditions
Challenges in Predicting Rotor Blade Ice Protection Coverage Extentusing Alternate Flow Solver and Lewice3D
Rotating Testing of a Low-Power, Non-Thermal Ultrasonic De-icingSystem for Helicopter Rotor Blades
FENSAP-ICE: 3D Simulation, and Validation, of De-icing with Inter-cycle Ice Accretion
Optimized Hot-Air Ice Protection Systems via FENSAP-ICE
Flight Tests in Natural Icing of the PZL Mielec M28 Commuter TurbopropAirplane
Shinan Chang, Beijing Univ. Aeronautics & Astronautics
Roger J. Aubert, Jason Wright, Bell Helicopter Textron
Austin Overmeyer, Jose Luis Palacios, Edward C. Smith, Penn State Univ.;Roger Royer, FBS Inc.
Thomas Reid, Guido S. Baruzzi, Isik A. Ozcer, Newmerical TechnologiesInc.; Wagdi G. Habashi, McGill Univ.
Mathieu Pellissier, Wagdi G. Habashi, McGill Univ.; Alberto Pueyo,Bombardier Aerospace
Mariusz Kubryn, Polskie Zaklady Lotnicze Sp. z o.o.; Robert Flemming,Sikorsky Aircraft Corp.; Ben Bernstein, Leading Edge Atmospherics; JanuszPietruszka, Polskie Zak¿ady Lotnicze Sp. z o.o.
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
10:30 a.m.
1:30 p.m.
Session Time:
Session Time:
Thursday, June 16
Thursday, June 16
Aircraft Anti-icing and Deicing Operations (Part 2 of 4)
Aircraft Anti-icing and Deicing Operations (Part 3 of 4)
Session Code:
Session Code:
ICE10
ICE10
Room Salon 3
Room Salon 3
This session addresses a wide variety of research topics related to aircraft ground deicing operations including active frost detection systems, liquidwater equivalent based systems to determine and update anti-icing fluid holdover times. Aircraft flight testing and wind tunnel testing with anti-icingfluids, along with fluid modeling, runway deicing fluid development and environmental regulations will also be discussed.
This session addresses a wide variety of research topics related to aircraft ground deicing operations including active frost detection systems, liquidwater equivalent based systems to determine and update anti-icing fluid holdover times. Aircraft flight testing and wind tunnel testing with anti-icingfluids, along with fluid modeling, runway deicing fluid development and environmental regulations will also be discussed.
Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration
Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration
Organizers -
Organizers -
Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration
Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration
Chairpersons -
Chairpersons -
8:30 a.m.
9:00 a.m.
9:30 a.m.
10:30 a.m.
11:00 a.m.
2011-38-0057
2011-38-0058
2011-38-0059
2011-38-0076
2011-38-0078
Transport Canada Guidelines for Aeroplane Testing FollowingDeicing/Anti-icing Fluid Application
Issues and Testing of Non-Glycol Aircraft Ground Deicing Fluids
A Comparison of an Automated Holdover Time Determination Algorithm(Checktime) to Outdoor Aircraft Anti-icing Fluid Testing
Cloud Phase Discrimination Using the Optical Icing Conditions Detector:Wind Tunnel and Flight Test Results
Wind Tunnel Experiments with Anti-Icing Fluids
James Martin, Transport Canada
Arlene Beisswenger, Caroline Laforte, Jean Perron, Anti-Icing Materials Intl.Laboratory
Scott Landolt, National Center for Atmospheric Research; Jennifer Black,NCAR; Roy Martin Rasmussen, National Center for Atmospheric Research
Kaare J. Anderson, Goodrich Advanced Sensors Technical Center; Gary E.Halama, Mark D. Ray, Goodrich Sensors & Integrated Systems; Michael P.Nesnidal, Goodrich Advanced Sensors Technical Center; Robert Ide, SierraLobo Inc. - NASA Glenn Research Center; Michael Poellot, David Delene,University of North Dakota
Michael Papadakis, Paul Strong, See-Cheuk Wong, Wichita State Univ.
ORAL ONLY
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
8:30 a.m.
10:30 a.m.
Session Time:
Session Time:
Thursday, June 16
Thursday, June 16
Aircraft Anti-icing and Deicing Operations (Part 4 of 4)
Test and Correlation (Part 1of 2)
Session Code:
Session Code:
ICE10
ICE7
Room Salon 3
Room Salon 6
This session addresses a wide variety of research topics related to aircraft ground deicing operations including active frost detection systems, liquidwater equivalent based systems to determine and update anti-icing fluid holdover times. Aircraft flight testing and wind tunnel testing with anti-icingfluids, along with fluid modeling, runway deicing fluid development and environmental regulations will also be discussed.
The test facilities session includes papers that describe ground icing test facilities (outdoor facilities, wind tunnels, and indoor cold chambers), detailmethods for the calibration of these facilites, present new ways to use these facilities, and that present data acquired in these facilities. Ice crystal andsupercooled large drop papers are in dedicated Appendix D and Appendix O sessions.
Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; James MacLeod, NationalResearch Council Canada
Organizers -
Organizers -
Oliver M. Arzt, N ICE Aircraft Services & Support GmbH; Warren M. Underwood, Federal AviationAdministration
James MacLeod, National Research Council Canada
Chairpersons -
Chairpersons -
11:30 a.m.
1:30 p.m.
2:00 p.m.
2:30 p.m.
8:30 a.m.
2011-38-0077
2011-38-0085
2011-38-0084
ORAL ONLY
ORAL ONLY
An Update on the Development of an Liquid Water Equivalent-basedSystem for Determining Precipitation Intensity
Laboratory Testing and Field Demonstration of an EnvironmentallyBenign and Reduced Corrosion Runway Deicing Fluid
Airport Deicing - Changing Environmental Regulations and AirportStrategies to Respond
Study of Ground Deicing Activities in European Airports
Ice Testing on Aerodynamic Surfaces
Roy Martin Rasmussen, Scott Landolt, National Center for AtmosphericResearch; Jennifer Black, NCAR; Andrew Gaydos, National Center forAtmospheric Research
Satya P. Chauhan, Melissa Roshon, W. D. Samuels, H. Nick Conkle,Battelle Memorial Institute; Elizabeth Berman, Mary Wyderski, US Air Force
Devon Seal, John Lengel, Timothy Arendt, Gresham Smith and Partners
Alberto Lopez, European Aviation Safety Agency
Stefan Jung, Domink Raps, Vuong Doan, Tobias Strobel, EADS GermanyGmbH
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
1:30 p.m.
8:30 a.m.
Session Time:
Session Time:
Thursday, June 16
Friday, June 17
Test and Correlation (Part 2 of 2)
Closing Plenary Session (Part 1 of 2)
Session Code:
Session Code:
ICE7
ICE13
Room Salon 6
Room Empire Ballroom
The test facilities session includes papers that describe ground icing test facilities (outdoor facilities, wind tunnels, and indoor cold chambers), detailmethods for the calibration of these facilites, present new ways to use these facilities, and that present data acquired in these facilities. Ice crystal andsupercooled large drop papers are in dedicated Appendix D and Appendix O sessions.
Robert J. Flemming, Sikorsky Aircraft Corp.; Richard Lewis, Airbus SAS; Mark G. Potapczuk, NASAGlenn Research Center
Organizers -
Mark G. Potapczuk, NASA Glenn Research CenterChairpersons -
Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research CenterModerators -
9:00 a.m.
9:30 a.m.
10:30 a.m.
11:00 a.m.
11:30 a.m.
8:30 a.m.
9:00 a.m.
9:30 a.m.
2011-38-0092
2011-38-0093
2011-38-0099
2011-38-0100
2011-38-0101
ORAL ONLY
ORAL ONLY
ORAL ONLY
An Experimental Correlation between Rotor Test and Wind Tunnel IceShapes on NACA 0012 Airfoils
Comparison of Experimental and Computational Ice Shapes for a SweptWing Model
Development of a Unique Icing Spray System for a New Facility forCertification of Large Turbofan Engines
Low Weight, Low Power, Electric Pulsed Deicer
S-76D¿ Tail Rotor Ice Impact Test
Inflight Icing Track Update
Icing Meteorology Track Update
Aircraft De/Anti-icing during Ground Operations Track Update
Yiqiang Han, Jose Luis Palacios, Edward C. Smith, Penn State Univ-University Park
See-Cheuk Wong, Michael Papadakis, Hsiung-Wei Yeong, See Ho Wong,Wichita State Univ.
James MacLeod, National Research Council Canada; John Jastremski,MDS Aero Support Corp.
Joseph J. Gerardi, Innovative Dynamics Inc.
Regina Kuznetsova, Sikorsky Aircraft Corp.
Robert J. Flemming, Sikorsky Aircraft Corp.
Ben C. Bernstein, Leading Edge Atmospherics
Warren Underwood, Federal Aviation Administration
ORAL ONLY
Time
Time
Paper No.
Paper No.
Title
Title
10:30 a.m.
8:30 a.m.
Session Time:
Session Time:
Friday, June 17
Closing Plenary Session (Part 2 of 2)Session Code: ICE13
Room Empire Ballroom
Richard Moser, Aerotex UK; Mark G. Potapczuk, NASA Glenn Research CenterModerators -
10:30 a.m. ORAL ONLY An FAA Update on Aircraft Icing
Thomas H. Bond, Federal Aviation Adminstration
Time Paper No. Title
10:30 a.m.Session Time: