Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds / Robert J. Mack.

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Bibliographic Details
Online Access:	Online Access
Main Author:	Mack, Robert J. (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1999.
Series:	NASA technical memorandum ; 1999-209534.
Subjects:	Aerodynamic characteristics. Body-wing configurations. Nacelles. Sonic booms. Wings. Aerodynamic configurations. Supersonic flight. Aerodynamic noise. Noise reduction. Wind tunnel tests.

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Call Number:	NAS 1.15:209534
NAS 1.15:209534	Available