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1
Terminal configured vehicle program : test facilities guide /
Washington, D.C. : Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1980

Book
2
Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method /
by Mohn, Larry Wayne
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book
3
Engine monitoring display study /
by Hornsby, Mary E.
Washington, D.C. : NASA, Scientific and Technical Information Program, 1992

Book
4
Dynamic loads analysis system (DYLOFLEX) summary.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979

Government Document Book
5
Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology /
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990

Government Document Book
6
Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings /
by Weatherill, W. H.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book
7
Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction /
by Pfenninger, W.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
8
Aerodynamic design and analysis system for supersonic aircraft /
by Middleton, W. D. (Wilbur D.), 1931-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book
9
Analysis of sonic boom measurements near shock wave extremities for flight near Mach 1.0 and for airplane accelerations /
by Haglund, George T. (George Thomas)
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
10
Cyclic debonding of adhesive joints : summary report /
by Hoffman, Daniel J.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book
11
Prediction of unsteady aerodynamic loadings caused by leading edge and trailing edge control surface motions in subsonic compressible flow : analysis and results /
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975

Government Document Book
12
A study to determine the feasibility of a low sonic boom supersonic transport /
by Kane, Edward J.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1973

Government Document Book
13
A computational system for aerodynamic design and analysis of supersonic aircraft /
by Middleton, W. D. (Wilbur D.), 1931-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1976

Book
14
Flow prediction for propfan engine installation effects on transport aircraft at transonic speeds /
by Samant, Satish S. (Satish Shripad), 1949-
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1986

Government Document Book
15
Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads /
by Viswanathan, A. V.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book
16
Analytical and experimental investigation of aircraft metal structures reinforced with filamentary composites /
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1971

Government Document Book
17
Natural laminar flow flight experiments on a swept wing business jet : boundary layer stability analyses /
by Rozendaal, R. A.
Washington, D.C : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1986

Government Document Book
18
4D-TECS integration for NASA TSRV airplane /
by Kaminer, I.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989

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Book
19
Terminal configured vehicle program : test facilities guide /
Washington, D.C. : Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1980

Government Document Book
20
The practical application of a finite difference method for analyzing transonic flow over oscillating airfoils and wings /
by Sebastian, J. D., Ehlers, F. Edward
[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
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