Research Catalog

Wind tunnel pressure study and Euler code validation of a missile configuration with 77̊ swept delta wings at supersonic speeds

Title
Wind tunnel pressure study and Euler code validation of a missile configuration with 77̊ swept delta wings at supersonic speeds [microform] / Patsy S. Fulton.
Author
Fulton, Patsy S.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]

Details

Additional Authors
Langley Research Center.
Description
vi, 115 p. : ill.
Series Statement
NASA technical memorandum ; 101531
Subject
  • Guided missiles > Aerodynamics
  • Angle of attack
  • Euler equations of motion
  • Missile configurations
  • Pressure distribution
  • Supersonic flow
  • Transonic flow
  • Wind tunnel models
  • Wind tunnel tests
Note
  • Cover title.
  • Distributed to depository libraries in microfiche.
  • "November 1988."
Bibliography (note)
  • Includes bibliographical references (p. 23).
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:101531
OCLC
marcive25698785
Author
Fulton, Patsy S.
Title
Wind tunnel pressure study and Euler code validation of a missile configuration with 77̊ swept delta wings at supersonic speeds [microform] / Patsy S. Fulton.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
Series
NASA technical memorandum ; 101531
Bibliography
Includes bibliographical references (p. 23).
Reproduction
Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1988] 2 microfiches : negative.
Added Author
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:101531
Research Call Number
READEX Microfiche NAS 1.15:101531
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