Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack /

Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack /

Bibliographic Details
Main Author: Latham, Eldon A. (Author)
Corporate Author: United States. National Aeronautics and Space Administration (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Moffett Field, California : Ames Research Center, May 1976.
Series:NASA technical memorandum ; X-73118.
Subjects:
Supersonic inlets.
Aerodynamics.
Mach number.
Jet engines > Air intakes.
Airplanes > Air ducts.
Air ducts > Aerodynamics.
Online Access:https://purl.fdlp.gov/GPO/gpo171204

Internet

https://purl.fdlp.gov/GPO/gpo171204

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Holdings details from Available Online
Call Number: NAS 1.15:X-73118
 
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NAS 1.15:X-73118 Available