Research Catalog

Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane

Title
Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane [microform] / Dennis O. Allision and William G. Sewall.
Author
Allison, Dennis O.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service (NTIS) [distributor, 1995]

Details

Additional Authors
  • Sewall, William G.
  • Langley Research Center.
Series Statement
NASA technical paper ; 3516
Subject
  • Aircraft models
  • Airfoils
  • Leading edges
  • Maneuverability
  • Pressure distribution
  • Subsonic speed
  • Trailing edges
  • Transonic speed
  • Wind tunnel tests
  • Wing-fuselage stores
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0744-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.60:3516
OCLC
marcive33953690
Author
Allison, Dennis O.
Title
Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane [microform] / Dennis O. Allision and William G. Sewall.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service (NTIS) [distributor, 1995]
Series
NASA technical paper ; 3516
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
Sewall, William G.
Langley Research Center.
Gpo Item No.
0830-H-15 (MF)
Sudoc No.
NAS 1.60:3516
Research Call Number
READEX Microfiche NAS 1.60:3516
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