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Navier-Stokes simulation of several high-lift reference H configurations [microform] / Wendy B. Lessard.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
1999
0 resources
Concept development of a Mach 2.4 high-speed civil transport [microform] / James W. Fenbert ... [et al.].
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Computations of axisymmetric flows in hypersonic shock tubes [microform] / Surendra P. Sharma and Gregory J. Wilson.
Microform
Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel [microform] / Richard J. Re and Francis J. Capone.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Measurements of supersonic wing tip vortices [microform] : 18th AIAA Aerospace Ground Testing Conference, June 20-23, 1994/Colorado Springs, CO / M.K. Smart, I.M. Kalkhoran and J. Bentson.
Microform
Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction [microform] : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV / by Jeffrey K. Wideman ... [et al.].
Microform
Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0 [microform] / Ramadas K. Prabhu ; [prepared ... under contract NAS1-96014].
Microform
Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
2001
0 resources
First order ozone impact of a fleet of supersonic business jets (SSBJs) [microform] / Steven L. Baughcum.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
2002
0 resources
Pilot comments for high speed research cycle 3 simulation study (LaRC.1) [microform] / Melvin L. Bailey, editor.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000]
2000
1 resource
Available online
Lee-side flow over delta wings at supersonic speeds [microform] / David S. Miller and Richard M. Wood.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
1985
0 resources
Optimal trajectories for an aerospace plane [microform] / by A. Miele, W.Y. Lee, and G.D. Wu.
Microform
Houston, Tex. : Rice University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
2 resources
Available online
Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A [microform] / James H. Dittmar.
Microform
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1985]
1985
0 resources
Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds [microform] / M. Leroy Spearman.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
1986
0 resources
Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design [microform] / V. Shankar and W.C. Clever.
Microform
Los Angeles, Calif. : Rockwell International Corporation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
1984
0 resources
Noise of the SR-6 propeller model at 2⁰ and 4⁰ angles of attack [microform] / James H. Dittmar, George L. Stefko, and Robert J. Jeracki.
Microform
[Washington, D.C. : National Aeronautics and Space Administration, 1983]
1983
0 resources