Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds
By: Robert J. Mack.
Contributors: Langley Research Center.
Series: [NASA technical memorandum] -- NASA/TM-1999-209534.; NASA technical memorandum -- 209534.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Body-wing configurations.; Nacelles.; Sonic booms.; Wings.; Aerodynamic configurations.; Supersonic flight.; Aerodynamic noise.; Noise reduction.; Wind tunnel tests.
Notes: Shipping list no.: 2000-0514-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000] 1 microfiche.