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

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

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Bibliographic Details
Main Author: Mack, Robert J.
Corporate Author: Langley Research Center
Format: Government Document Microfilm Book
Language:English
Published: Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1999]
Series:NASA technical memorandum ; 209534.
Subjects:
Aerodynamic characteristics.
Body-wing configurations.
Nacelles.
Sonic booms.
Wings.
Aerodynamic configurations.
Supersonic flight.
Aerodynamic noise.
Noise reduction.
Wind tunnel tests.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number: NAS 1.15:209534
NAS 1.15:209534 Restricted Place a Hold

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