Research Catalog

Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds

Title
Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds [microform] / Gloria Hernandez ... [et al.].
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

Details

Additional Authors
  • Hernandez, Gloria.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 4542
Alternative Title
Effect of leading and trailing edge flaps on clipped delta wings with and without wing camber at supersonic speeds
Subject
  • Aerodynamic characteristics
  • Angle of attack
  • Delta wings
  • Leading edge flaps
  • Mach number
  • Supersonic speed
  • Thin wings
  • Trailing edge flaps
  • Twisted wings
  • Uncambered wings
  • Wind tunnel tests
  • Wing camber
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:4542
OCLC
marcive32143625
Title
Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds [microform] / Gloria Hernandez ... [et al.].
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
Series
NASA technical memorandum ; 4542
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 2 microfiches.
Added Author
Hernandez, Gloria.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:4542
Research Call Number
READEX Microfiche NAS 1.15:4542
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