Experimental investigation of wing installation effects on a two-dimensional mixer/ejector nozzle for supersonic transport aircraft

Experimental investigation of wing installation effects on a two-dimensional mixer/ejector nozzle for supersonic transport aircraft

Bibliographic Details
Main Author: Anderson, David J
Corporate Author: United States National Aeronautics and Space Administration
Other Authors: Lambert, Heather H, Mizukami, Masashi
Format: Government Document Book
Language:English
Published: [Washington, D.C.] : [Springfield, Va. : NASA ; National Technical Information Service, distributor, 1992]
Series:NASA technical memorandum 105713
Subjects:
Acoustic properties
Ejectors
Engine airframe integration
Exhaust nozzles
Flow distribution
Inlet flow
Noise reduction
Nozzle flow
Supersonic transports
Wind tunnel tests
Wings

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Stanford University

Holdings details from Stanford University
Call Number: ISIL:US-CST
MARCIVE
NAS 1.15:105713

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