Research Catalog

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

Title
Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds [microform] / Robert J. Mack.
Author
Mack, Robert J.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]

Details

Additional Authors
Langley Research Center.
Description
1 v.
Series Statement
[NASA technical memorandum] ; NASA/TM-1999-209534
Uniform Title
NASA technical memorandum ; 209534.
Subject
  • Aerodynamic characteristics
  • Body-wing configurations
  • Nacelles
  • Sonic booms
  • Wings
  • Aerodynamic configurations
  • Supersonic flight
  • Aerodynamic noise
  • Noise reduction
  • Wind tunnel tests
Note
  • Shipping list no.: 2000-0514-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:209534
OCLC
marcive43917968
Author
Mack, Robert J.
Title
Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds [microform] / Robert J. Mack.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
Series
[NASA technical memorandum] ; NASA/TM-1999-209534
NASA technical memorandum ; 209534.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000] 1 microfiche.
Added Author
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:209534
Research Call Number
READEX Microfiche NAS 1.15:209534
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