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Recent applications of theoretical analysis to V/STOL inlet designThe theoretical analysis methods, potential flow, and boundary layer, used at Lewis are described. Recent application to Navy V/STOL aircraft, both fixed and tilt nacelle configurations, are presented. A three dimensional inlet analysis computer program is described and preliminary results presented. An approach to optimum design of inlets for high angle of attack operations is dicussed.
Document ID
19790020972
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stockman, N. O. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
E-096
NASA-TM-79211
Report Number: E-096
Report Number: NASA-TM-79211
Meeting Information
Meeting: Workshop on V/STOL Aerodyn.
Location: Monterey, CA
Country: United States
Start Date: May 16, 1979
End Date: May 18, 1979
Sponsors: Naval Air Develop. Center
Accession Number
79N29143
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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