scope and aimmaltutty.com/content/reference material/aiac 2015-022 … · · 2015-09-20scope and...
TRANSCRIPT
Scope and Aim
*Identify aircraft stores separation in the
context of MIL-STD/HDBK-1763 and 244A and
establishing aircraft stores compatibility
*Revisit Applied CFD Challenge II after 15 years
*Discuss joint fires future:
*the profession of arms in the Information Age
*establishing armament systems compatibility
*JAIME CODEx
*But first: imagery on the
Presenters’ Backgrounds …
Unclassified Unclassified 2
S
OUTH AUSTRALIA
WO
OM
ER
A
TEST RANGE
Unclassified
P>x = δ x -π
Peta JMPIs
Serviced
(0<x<1)
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Terminology
* ACFD. Applied Computational Fluid Dynamics
* AIME. Armament Integrated Mission Environment.
* ASC. Armament Systems Compatibility.
* Fires. The use of weapon systems to create a specific lethal or nonlethal effect on a target.
* Information Age. In the post-digital age, the benchmark is the use of distributed modelling and simulation in a Live, Virtual and Constructive (LVC) environment.
* Joint Fires. Fires applied during the employment of forces from two or more components, in coordinated action toward a common objective.
* Profession of Arms. Traditionally seen as those personnel who are uniformed members of a professional military force. The authors view – those personnel who are professionally involved in live trials, experimentation and the employment of arms: when used to destroy or neutralise threats be they kinetic, non-kinetic or cyber-based.
* Threats. The ability of an enemy, or potential enemy, person, organization or physical object/entity that intends to cause harm (i.e., limit, neutralise, or destroy effectiveness of current or projected mission, organization, or item of equipment).
* Yin-Yang. Literally shadow and light / female and male
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ALITITUDE ( ft)
30,000
0.4 0.6 0.8 1.0 1.1 1.2
MACH NUMBER
700KCAS
600 KCAS
500 KCAS
400 KCAS
300 KCAS
CARRIAGE
EMPLOYMENT
0.90.70.50
0
20,000
10,000
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• PART I – FUNCTIONAL DESCRIPTION
• PART II – FORM, FIT AND FUNCTION
• PART III – STRUCTURAL AND ENVIRONMENTAL
• PART IV – AEROELASTICITY
• PART V – CAPTIVE CARRIAGE: HANDLING QUALITIES AND PERFORMANCE
• PART VI – EMPLOYMENT AND JETTISON
• PART VII – MISSION PLANNING, BALLISTICS, SAFE ESCAPE AND WEAPON DANGER AREAS
• PART VIII – PROCEDURE
- 1 Operators / Flight Manual
- 2 System Preparation / Maintenance Manual
- 3 Systems Loading Manual
- 4 Tactics Manual
- 5 Mission Planning Tools
• PART IX – SPECIFICATIONS
Aircraft Stores Compatibility
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The Standard Top Ten Lies to Engineering
1. It’s only a software change.
2. It’s the same as a MK82 / AIM-9 / MJU-8 *.
3. Only secondary structure was modified.
4. The Contractor / Project Office / Cleaner * says its OK.
5. The US Army / Air Force / Navy / Brits / Canadians * do it all the time ...
6. The OT&E starts today, we don’t need a Clearance then do we?
7. It’s just a “one-time” flight, we don’t need a Clearance then ...
8. This Program has CAF’s top priority, we don’t need ...
9. Of course there’s an agreed Operational Concept ...
10. I’ll still respect you after the flight.
* Select any one, it doesn’t really matter
Unclassified Armament Systems Compatibility: Mal Tutty Unclassified 7
Unclassified 8
JDAM FLIGHT 13M = 0.962 6382 FT 43 DIVE
FIGURE 3 JDAM MISS DISTANCE
0 0.05 0.1 0.15 0.2 0.25
TIME, SEC
0
5
10
15
20
25INCHES
PREDICTION
TEST PHOTOGRAMETRICS
TEST TELEMETRY
JDAM FLIGHT 14M = 1.055 10832 FT 44 DIVE
FIGURE 4 JDAM MISS DISTANCE
0 0.04 0.08 0.12 0.16 0.2 0.24
TIME, SEC
0
4
8
12
16
20INCHES
PREDICTION
TEST PHOTOGRAMETRICS
TEST TELEMETRY
JDAM FLIGHT 13
M = 0.962 6382 FT 43 DIVE
FIGURE 1 JDAM ATTITUDES
0 0.05 0.1 0.15 0.2 0.25
TIME, SEC
0
5
-5
-10
-15
-20
DEG
TELEMETRY
PREDICTION
THE
PSI
PHI
JDAM FLIGHT 14M = 1.055 10832 FT 44 DIVE
FIGURE 2 JDAM TRAJECTORY
0 0.05 0.1 0.15 0.2 0.25
TIME, SEC
0
5
-5
-10
-15
-20
DEG
TELEMETRY
PREDICTION
THE
PSI
PHI
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JDAM FLIGHT 13M = 0.962 6382 FT 43 DIVE
FIGURE 11 JDAM TRAJECTORY
0 0.05 0.1 0.15 0.2 0.25
TIME, SEC
0
5
-5
-10
-15
-20
-25
DEG
TELEMETRY
PREDICTION RAMPANT
THE
PSI
PHI
JDAM FLIGHT 14M = 1.055 10832 FT 44 DIVE
FIGURE 12 JDAM ATTITUDES
0 0.05 0.1 0.15 0.2 0.25
TIME, SEC
0
5
-5
-10
-15
-20
DEG
TELEMETRY
PREDICTION RAMPANT
THE
PSI
PHI
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Distribution of aircraft and store
geometries and flight test data
Quality of papers and presentations.
Representative of state of the art for
current CFD-based tools for stores
carriage and separations.
Wind tunnels will still be relied on for the
provision of the major part of the
aerodynamic data on which stores
certification are to be based.
CFD solutions were within the error range
of the wind tunnel and flight test data.
Accuracy would not be the issue.
Time required to produce a solution needs
to be decreased significantly.
CFD-based tools should now become far
more prevalent in use during
Requirements Definition and Systems
Engineering trade-off studies.
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Improvements in the ejector modeling and
ejector foot/store interaction during the
ejection needed to be accomplished.
One of the principal drawback of CFD
Challenge II was that all the CFD results,
using both Euler and Navier Stokes, as
well as a simulation that ignored the
JDAM canards gave similar results.
Does that mean that Navier Stokes
formulation does not have to be used, or
were the test cases selected fortuitous for
the inviscid formulation?
ACFD III warranted to investigate.
Results available from
www.maltutty.com and
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Comparison of PSP test data with CFD predictions
F-18/MK-83 BL 143 store CP M = 0.90 a = 4.5
-0.80
-0.60
-0.40
-0.20
0.00
0.20
0.40
0.60
0.80
1.00
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
x/c
Australia
Canada
PSP
US Navy
UK
Pre
ssu
re
coe
ffici
ent,
Cp
Normalised chordwise distance, x/c
F-18/MK-83 BL 143 store CP M = 0.90 a = 4.5
-0.80
-0.60
-0.40
-0.20
0.00
0.20
0.40
0.60
0.80
1.00
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
x/c
Australia
Canada
PSP
US Navy
UK
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-25
-20
-15
-10
-5
0
5
10
15
20
25
30
0.00 0.04 0.08 0.12 0.16 0.20 0.24 0.28 0.32 0.36 0.40
De
gre
es
time
MK-84/Litening M = 0.93 570 KCAS
The telemetry
Psi
Phi
The Prediction
Psi
Phi
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Unclassified 21
The Profession of Arms in the Information Age:
network enabled armament systems compatibility in an LVC world
AIAC 2015, METU Ankara Turkey, 11 September 2015
Malcolm ‘Maven’ Tutty MEng, FIE(Aust), RAeS JAIME Enterprises Australia
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Live
Embedded Training Systems C4I &
Combat
Systems
Role Players
Exercise Control
AAR
Response Cells
Opposing Force
(OPFOR)
Design
Plan Prepare Execute
Analyze Evaluate
Knowledge Management
Assets
Authoritative Sources
Joint LVC Testing & Training Environment Testing & Training Audience
Joint, Multinational, & Coalition Partners
Global Information
Grid
Joint Coalition Context
Virtual
Constructive
Planners & Designers
Key Players: JMETC
InterTEC Test Community
Training Community
Instru
me
nta
tion
TE
NA
& C
RIIS
McKee SETE 2010
Armament Systems Compatibility: Mal Tutty Unclassified 23
A Family of System of Systems
Unclassified
Systems – The Platform, Flight &
Mission Sim, SE Integ Lab, PT Trnrs
FoS - Σ SoS for the JTF
SoS – Σ Platform Type(s) +
Flight & Mission Sims +
SE Integ Lab + LVC + TENA +
Part Task Trainers +
Weapons +
EW / DE / EWSP +
TBMCS + Missions Planning +
Intell + Maintenance + …
Developed at Tutty (2012) from Abbott (2009) Unclassified 25
• PART I – PHYSICAL SUITABILITY: CONCEPTUAL & FUNCTIONAL DESCRIPTION
• PART II – PHYSICAL SUITABILITY: FORM & FIT
• PART III – PHYSICAL SUITABILITY: STRUCTURAL AND ENVIRONMENTAL
• PART IV – PHYSICAL SUITABILITY: AEROELASTICITY
• PART V – PHYSICAL SUITABILITY: CAPTIVE CARRIAGE: HANDLING QUALITIES AND PERFORMANCE
• PART VI – PHYSICAL SUITABILITY: EMPLOYMENT AND JETTISON – NOISE & EM EMISSIONS & RCS
• PART VII – INFORMATION SUITABILITY: EXTERNAL INTERFACES, MISSION PLANNING, BALLISTICS, SAFE
ESCAPE, WEAPON DANGER AREAS AND MUNITIONS EFFECTIVENESS
• PART VIII – COGNITIVE SUITABILITY: PROCEDURES, TTPS AND HUMAN FACTORS
- 1 Operators / Flight Manual
- 2 System Preparation / Maintenance Manual
- 3 Systems Loading Manual
- 4 Tactics Manual
- 5 Mission Planning Tools
• PART IX – EMERGENT PROPERTIES: COI/CTP/MOE/MOP TEST AND EXPERIMENTATION
• PART X – SPECIFICATIONS TRACEABILITY
Armament Systems Compatibility
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Conclusions
Unclassified
Aircraft Stores Compatibility history
Need for Wind Tunnels usage questioned in 1980/90s
Confidence in CFD usage for timely aircraft stores separation
and inserted early in weapons integration program
Bottom Line: ACFD II Challenge Blind Tests established CFD
accuracy and confidence for aircraft stores separation use
Next: Pt II on Armament Systems Compatibility and Pt III aircraft
stores handling qualities, performance and accuracy testing
Network-enabled complex adaptive systems impact …
Five Eyes / NATO Code of Practice proposed for Experimenters
and Testers to establish network-enabled Armament Systems
Compatibility
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Unclassified -3
Si ego Certiorem Faciam, Mihi Tu Delendus Eris. Homer, The Iliad
Disclaimer
*The research & presentation are derived from research
primarily based on unclassified, open sources: see AIAC-2015-
022 paper at Tutty etal (2015), available from 8th AIAC and the
authors website – www.maltutty.com
*Author’s views are based on ongoing research in the Five Eyes
and NATO and are intended to promote discussion.
*The results are Unclassified, publically releasable but do not
necessarily represent the extant official views of the
Australian / US Department of Defence, the Five Eye nations
or that of University of SA, as yet.
*No apologies about the HIGH ‘Augustine Acronym Index’ –
if you can’t translate these ones as engineers, scientists or
techo wannabes you really shouldn’t be playing in the military
effects-based space!
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