Experimental evaluation of a spinning-mode acoustic-treatment design concept for aircraft inlets/
Main Author: | Heidelberg, Laurence J. |
---|---|
Corporate Authors: | United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lewis Research Center |
Other Authors: | Rice, Edward J., Homyak, Leonard |
Format: | Book |
Language: | English |
Published: |
Washington, D.C.:
National Aeronautics and Space Administration, Scientific and Technical Information Office,
1980
|
Series: | NASA technical paper
1613 |
Subjects: |
Similar Items
-
Aerodynamic and directional acoustic performance of a scoop inlet/
by: Abbott, John M.
Published: (1977) -
Simulated flight effects on noise characteristics of a fan inlet with high throat Mach number/
by: Wesoky, Howard L.
Published: (1978) -
Jet aircraft power systems : principles and maintenance /
Published: (1950) -
Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry, supersonic inlet configuration/
by: Hawkins, J. E.
Published: (1976) -
Airflow and thrust calibration of an F100 engine, S/N P680059, at selected flight conditions/
by: Biesiadny, Thomas J.
Published: (1978)