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Sonic inlet technology development and application to STOL propulsionRecent developments in sonic inlet technology are presented with particular emphasis on STOL propulsion systems. Inlet noise reduction requirements are considered for an augmentor wing and an upper surface blowing type of propulsion system. The current state of the art is discussed with respect to performance and noise potential of different sonic inlet concepts. An acoustic and aerodynamic performance comparison is presented for several inlet configurations based on experimental results.
Document ID
19740052231
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klujber, F.
Okeefe, J. V.
(Boeing Commercial Airplane Co. Renton, Wash., United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1974
Subject Category
Aircraft
Report/Patent Number
SAE PAPER 740458
Report Number: SAE PAPER 740458
Meeting Information
Meeting: Air Transportation Meeting
Location: Dallas, TX
Start Date: April 30, 1974
End Date: May 2, 1974
Sponsors: Society of Automotive Engineers
Accession Number
74A34981
Distribution Limits
Public
Copyright
Other

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