Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /

Bibliographic Details

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.
Online Access:	https://purl.fdlp.gov/GPO/gpo84509