Search Results

181

Aerothermal and structural performance of a cobalt-base superalloy thermal protection system at Mach 6.6 /

by Sawyer, James Wayne
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book

182

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /

by Pittman, Jimmy L.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

183

Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards /

by Robins, A. Warner, Lamb, Milton, Miller, David S.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Office, 1979

Government Document Book

184

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 s̊wept double-delta wing at Mach number 0.2 /

by Penland, Jim A., Creel, Theodore R., Dillon, James L.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978

Government Document Book

185

Aerodynamic characteristics at Mach numbers from 0.33 to 1.20 of wing-body design concept for a hypersonic research airplane /

by Dillon, James L., Pittman, Jimmy L.
[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977

Government Document Book

186

Experimental performance of an ablative material as an external insulator for a hpersonic research aircraft /

by Puster, Richard L., Chapman, Andrew J.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book

187

Investigation of effect of propulsion system installation and operation on aerodynamics of an airbreathing hypersonic airplane at Mach O.3 to 1.2 /

by Cubbage, James M., Mercer, Charles E. (Aerospace engineer)
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book

188

Downstream influence of swept slot injection in hypersonic turbulent flow /

by Hefner, Jerry N., Carey, Aubrey M., Bushnell, Dennis M.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book

189

Aerodynamic characteristics of two single-stage-to-orbit vehicles at Mach 20.3 /

by Bernot, Peter T.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book

190

Ambient temperature fatigue tests of elements of an actively cooled honeycomb sandwich structural panel /

by Sharpe, Ellsworth L., Elber, Wolf
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book

191

Flightweight radiantly and actively cooled panel : thermal and structural performance /

by Shore, Charles P.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982

Government Document Book

192

Aerodynamic characteristics, including effect of body shape, of a Mach 6 aircraft concept /

by Riebe, Gregory D.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book

193

Validation of scramjet exhaust simulation technique at Mach 6 /

by Hopkins, H. B.
Washington : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1979

Government Document Book

194

Loading tests of a wing structure for a hypersonic aircraft /

by Fields, Roger A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980

Government Document Book

195

Actively cooled plate fin sandwich structural panels for hypersonic aircraft /

by Smith, L. M. (Lee Mark)
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979

Government Document Book

196

Preliminary scramjet design for hypersonic airbreathing missile application /

by Carlson, Charles H.
Washington, D.C. : [Springfield, VA.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983

Government Document Book

197

Analysis of various descent trajectories for a hypersonic-cruise, cold-wall research airplane /

by Lawing, Pierce L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

198

Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 s̊wept delta wing /

by Penland, Jim A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book

199

Performance of a hypersonic hot fuselage structure with a carbon dioxide frost protected, nonintegral cryogenic tank /

by Sharpe, Ellsworth L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

200

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 s̊wept double-delta wing at Mach numbers from 1.50 to 2.86 /

by Penland, Jim A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book

Narrow Search