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1

Isolated rotor noise due to inlet distortion or turbulence /

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

Government Document Book

2

Study of noise sources in a subsonic fan using measured blade pressures and acoustic theory /

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

Government Document Book

3

General design method for three-dimensional potential flow fields /

by Stanitz, John D.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Techincal Information Service, 1980

Government Document Book

4

Streamline curvature design procedure for subsonic and transonic ducts /

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

Government Document Book

5

Combined quadrupole-dipole model for inlet flow distortion noise from a subsonic fan /

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

Government Document Book

6

Three-dimensional compressible turbulent computations for a diffusing S-duct /

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

Government Document Book

7

Experimental evaluation of a Mach 3.5 axisymmetric inlet /

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

Government Document Book

8

A parametric study of effect of forebody shape on flow angularity at Mach 8 /

by Johnson, Charles B. (Charles Borden), 1931-2019
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book

9

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of a translating-grid choked-flow inlet /

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

Government Document Book

10

Pressure distributions for a rectangular supersonic inlet at subsonic speeds /

by Fuller, Dennis E.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1976

Government Document Book

11

Model investigation of inlet plenum flow straightening techniques for altitude test facility /

by Riddlebaugh, Stephen M.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1976

Government Document Book

12

Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet /

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

Government Document Book

13

Terminal-shock and restart control of a Mach 2.5, mixed-compression inlet coupled to a turbofan engine /

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

Government Document Book

14

Terminal-shock and restart control of a Mach 2.5, axisymmetric, mixed compression inlet with 40 percent internal contraction /

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

Government Document Book

15

Analysis of pressure distortion testing /

by Koch, K. E., Rees, R. L.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976

Government Document Book

16

Optimal one-section and two-section circular sound-absorbing duct liners for plane-wave and monopole sources without flow /

by Lester, Harold C., Posey, Joe W.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976

Government Document Book

17

Study of noise and inflow distortion sources in the NASA QF-1B fan using measured blade and vane pressures /

by Hanson, Donald, B.
Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977

Government Document Book

18

Prediction of laminar and turbulent primary and secondary flows in strongly curved ducts /

by Kreskovsky, J. P.
Washington, D.C. : Springfield, Va. : National Aernautics and Space Administration, Scientific and Technical Information Branch ; For sale by National Technical Information Service, 1981

Government Document Book

19

Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations /

by Hayes, Clyde
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

20

Nonlinear effects on sound propagation through high subsonic Mach number flows in variable area ducts /

by Callegari, Andrew John
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1979

Government Document Book

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