Search Results

1

Heat transfer from cylinders in subsonic slip flows /

by Nagabushana, K. A., 1958-
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992

Government Document 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

TRANDESNF : a computer program for transonic airfoil design and analysis in nonuniform flow /

by Chang, Jen-Fu
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987

Government Document Book

4

Evaluation of flow properties behind 120-̊ and 140-̊included-angle cones and a Viking '75 entry vehicle at Mach numbers from 1.60 to 3.95 /

by Brown, Clarence A.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

5

The measurement of disturbance levels in the Langley Research Center 20-inch Mach 6 tunnel /

by Stainback, P. C.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994

Government Document Book

6

Inverse boundary-layer theory and comparsion with experiment /

by Carter, James E. (James Edward), 1944-
Washington, DC : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.

Government Document Book

7

Deployment and performance characteristics of 1.5-meter supersonic attached inflatable decelerators /

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

Government Document Book

8

Numerical analysis and simulation of an assured crew return vehicle flow field /

by Weilmuenster, K. James
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; For sale by the National Technical Information Service, 1991

Government Document Book

9

Improvements to the missile aerodynamic prediction code DEMON3 /

by Dillenius, Marnix F. E., 1938-
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992

Government Document Book

10

Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction /

by Micol, John R.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992

Government Document Book

11

Improved method for prediction of attainable leading-edge thrust /

Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; Available from the National Technical Information Service, 1996

Book

12

Wind-tunnel investigation at low speeds of a model of the Kestrel (XV-6A) vectored-thrust V/STOL airplane /

by Margason, Richard J. (Richard John), 1936-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972

Government Document Book

13

Bibliography on aerodynamics of airframe/engine integration of high-speed turbine-powered aircraft /

by Nichols, Mark R.
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

Vortex flow aerodynamics : proceedings of a conference /

Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986

Book

15

Dynamic loads analysis system (DYLOFLEX) summary.

Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1979

Government Document Book

16

Exploratory wind-tunnel study of the aerodynamic characteristics of a generic accelerator-type configuration at low subsonic speeds /

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1988

Book

17

Review of propulsion-induced effects on aerodynamics of jet/stol aircraft /

by Margason, Richard J. (Richard John), 1936-
Washington : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Va.], 1970

Government Document Book

18

Noise and wake structure measurements in a subsonic tip speed fan /

Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book

19

Further analysis of broadband noise measurements for a rotating blade operating with and without its shed wake blown downstream /

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

Government Document Book

20

Effects of jet-exhaust location on the longitudinal aerodynamic characteristics of a jet V/STOL model /

by Carter, Arthur W.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1969

Government Document Book

Narrow Search