Search Results

1

A System for aerodynamic design and analysis of supersonic aircraft.

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

2

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8° to 90° /

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

3

Aeroelastic loads prediction for an arrow wing /

Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983

Government Document Book

4

Electric flight systems : proceedings of a workshop held in Hampton, Virginia, June 9-10, 1981 /

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

Book

5

Theoretical and experimental investigation of ground-induced effects for a low-aspect-ratio highly swept arrow-wing configuration /

by Coe, Paul L.
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

6

Simulation comparison of a decoupled longitudinal control system and a velocity-vector control wheel steering system during landings in wind shear /

by Miller, G. Kimball
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

7

Dynamic response of a forward-swept-wing model at angles of attack up to 15 at a Mach number of 0.8 /

by Doggett, Robert V.
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

8

A new theory for rapid calculation of the ground pattern of the incident sound intensity produced by a maneuvering jet airplane /

by Barger, Raymond L.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

9

Aerothermal analysis of a wing-elevon cove with variable leakage /

by Hunt, L. Roane (Lewis Roane)
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

10

Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds /

by Carlson, Harry W.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

11

Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 /

by Hunt, L. Roane (Lewis Roane)
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

12

Rotary balance data for a single-engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 t̊o 90 /̊

by Mulcay, William
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

13

Induced drag ideal efficiency factor of arbitrary lateral-vertical wing forms /

by DeYoung, John
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

14

A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise /

by Grantham, William D.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

15

Thermal-structural design study of an airframe-integrated scramjet : summary report /

by Buchmann, O. A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Information Service], 1979

Government Document Book

16

Development and test results of a flight management algorithm for fuel-conservation descents in a time-based metered traffic environment /

by Knox, Charles E.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

17

Dual methods and approximation concepts in structural synthesis /

by Fleury, Claude
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

18

Leading-edge deflection optimization for a highly swept arrow-wing configuration /

by Coe, Paul L.
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980

Government Document Book

19

Parametric study of microwave-powered high-altitude platforms designed for linear flight /

by Morris, Charles E. K.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book

20

Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations /

by Kumar, Ajay
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981

Government Document Book

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