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daa-1099.pdfmark woodardu>, david fo1ta, dennis woodfork m nasajgsfc, greenbelt, md-20771 usa, +l 301.286.9611, [email protected] nasaigsfc,
m u l t i d i s c i p l i n a r y research a c t i v i t y i n t h e ma te r ia l s sciences w i t h emphasis on ceramic m a t e r i a l s nasa research grant number nsg-484
yrpa182.pdfno . 992 strengw ol? aircrax’t wing structures b,y hans w: ka.ui (/ ,, statistical analys.is of the t~me and fatigue strength of aircraft wing structures*
submitted by houston, texas 77058 project summary a novel adaptive fuzzy system using the concept of the adaptive resonance theory (art) type neural network architecture
under-the-wing engine composite fan blade final des ign test report february 1977 advanced engineering & technology programs departmen: g e n e r a l e l e c t r i c
2005009811.pdfchanged byal- - - -----date =^z= altitude starting tests of a 1000-pound-thrust solid-propellant rocket by john l. sloop, r. james rollbuhler, and eugene m.
ff 653 july 65 march 1968 report no. 68-10 researches in optimal and suboptimal control t h e o r y report no. 68-10 march 1968 g. kang los angeles the research described
19840021771august 1984 ni\s/\ j. b. plescia, compiler ni\s/\ national aeronautics and space administration scientific and technical information branch 1984 contents page
in space by: a. l. berlail state university of h e w pork at stony brook - 1 george h. hrkatcin factory mutual research corporation noward b. palmer penfisglvada state uaiversity
wha t if things get worse? really grand challenges for modeling and simulation in a risky and complex world or act 1: setting the stage today modeling and simulation-- ---as
19820016265april 1982 ni\s/\ and their associates, 1980-1981 joseph m. boyce, compiler nasa office of space science and applications washington, d.c. ni\s/\ national aeronautics
philip mason, edwin lerner, and lawrence sobel grumman aircraft systems division grumman corporation bethpage, new york preceding page blank not rlmfd 3 4 introduction many
ssti-2200-0110.ppt.pdfow acknowledgements the author wishes to acknowledge the nasa innovative partnerships program (ipp) for supporting the development of the technologies
study of design and control of remote manipulators part ii vibration considerations in manipulator design wayne j. book nasa contract nas8-28055 marshall space flight center
n95- 14247 high angle of attack flying qualities criteria for longitudinal rate command systems david j. wilson and kevin d. citurs mcdonnell douglas aerospace mcdonnell
20101103114237
* the spontaneous i o n i z a t i o n of a hydrogen atom i n an electric field, i .f. joseph 0. hi rschfe lder and larry a. cur t i s s univers i ty of wisconsin theore t
memorandum february 5, 1965 a~ - -- transient pressure response in a fluid system as a vibrating valve closes by cecil a. ponder, jr. propulsion and vehicle engineering laboratory
a9re966.tmpshape memory alloy self-healing {smash) technology investigators: m. clara wright, nasa ksc1 michele manuel, university of florida2 terryl wallace, nasa larc3
louis j. goldman national aeronaut ics and space administratio11 lewis research center cleveland, ohio abs tract methods f o r designing supersonic s t a t o r and r o t