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Variable geometry requirements in inlets and exhaust nozzles for high Mach number applications.Variable geometry supersonic aircraft design, discussing inlet and exhaust nozzles problems and wind tunnel tests
Document ID
19680058252
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Beheim, M. A.
Boksenbom, A. S.
Date Acquired
August 4, 2013
Publication Date
September 1, 1968
Publication Information
Publisher: INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES,
Subject Category
Aerodynamics
Report/Patent Number
ICAS PAPER 68-20
Report Number: ICAS PAPER 68-20
Meeting Information
Meeting: INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES, CONGRESS
Location: MUNICH
Country: GERMANY
Start Date: September 9, 1968
End Date: September 13, 1968
Accession Number
68A39224
Distribution Limits
Public
Copyright
Other

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