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United States National Aeronautics and Space Administration8Langley Research Center6Calise, Anthony J.2United States National Aeronautics and Space Administration > Scientific and Technical Information Branch2Braswell, Dorothy O.1Chudoba, Bernd1Cox, Timothy H.1Dahl, Milo D., 1956-1Dillon, James L.1Driver, Cornelius1 more »
NASA technical memorandum5NASA contractor report4NASA technical paper3Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.01Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.861Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.631Fail-safe system for actively cooled supersonic and hypersonic aircraft1A flying qualities study of longitudinal long-term dynamics of hypersonic planes1Forces due to air and helium jets impinging normal to a flat plate for near-vacuum and sea-level ambient pressures1NASA contractor report; NASA CR-1865711 more »
Hypersonic aircraft13Aerodynamic characteristics4Aerodynamics3Hypersonic planes3Supersonic aircraft3Aerodynamic configurations2Aerodynamic stability2Aircraft stability2Computational fluid dynamics2Computer programs2 more »

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Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation [1996]

Ko, William L.; United States National Aeronautics and Space Administration > Scientific and Technical Information Program
E-Book
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996
NAS 1.15:4770
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