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Inlet-engine-nozzle wind tunnel test techniquesSupersonic propulsion system inlet, engine and exhaust nozzle in wind tunnel and flight tests, discussing boundary layer effects on performance
Document ID
19710062902
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bowditch, D. N.
Date Acquired
August 6, 2013
Publication Date
September 1, 1971
Subject Category
Propulsion Systems
Meeting Information
Meeting: MEETING OF THE PROPULSION AND ENERGETICS PANEL
Location: SANDEFORD
Country: NORWAY
Start Date: September 13, 1971
End Date: September 17, 1971
Sponsors: NATO, AGARD
Accession Number
71A43599
Distribution Limits
Public
Copyright
Other

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