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Inlet technology for powered-lift aircraftThe concepts, analytical tools, and experimental data available for designing inlets for powered lift aircraft are discussed. It is shown that inlets can be designed to meet noise, distortion, and cruise drag requirements at the flight and engine operating conditions of a powered lift aircraft. The penalty in pressure recovery for achieving the required noise suppression was 0.3 percent.
Document ID
19780016126
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Luidens, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Powered-Lift Aerodyn. and Acoustics
Subject Category
Aerodynamics
Accession Number
78N24069
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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