Analytical and experimental studies of acoustic performance of segmented liners in a compressor inlet /
R.E. Motsinger ... [et al.].

Description

Related Names

Motsinger, R. E.
General Electric Company.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington : National Aeronautics and Space Administration ; 1977.

Subjects

Compressors > Compressors / Aerodynamics.
Airplanes > Airplanes / Turbofan engines > Airplanes / Turbofan engines / Noise.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Mufflers.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Compressors > Airplanes / Turbojet engines / Compressors / Noise.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Air intakes > Airplanes / Turbojet engines / Air intakes / Noise.

Note

Issued Sept. 1977.
Prepared by General Electric Company under contract no. NAS1-13416.

Physical Description

xvi, 132 p. : ill. ; 27 cm.

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