Research Catalog

Hypersonic boundary-layer transition for X-33 phase II vehicle

Title
Hypersonic boundary-layer transition for X-33 phase II vehicle [microform] / R.A. Thompson ... [et al.].
Publication
Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]

Details

Additional Authors
  • Thompson, R. A.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
[NASA technical memorandum] ; 207316
Alternative Title
Hypersonic boundary layer transition for X-33 phase 2 vehicle
Subject
  • Boundary layer transition
  • Hypersonics
  • Flow distribution
  • Wind tunnel tests
  • Finite volume method
  • Flow visualization
Note
  • Shipping list no.: 99-0199-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:207316
OCLC
marcive40771865
Title
Hypersonic boundary-layer transition for X-33 phase II vehicle [microform] / R.A. Thompson ... [et al.].
Imprint
Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
Series
[NASA technical memorandum] ; 207316
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.
Added Author
Thompson, R. A.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:207316
Research Call Number
READEX Microfiche NAS 1.15:207316
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