Research Catalog

High Reynolds number test of the Boeing TR77 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

Title
High Reynolds number test of the Boeing TR77 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel [microform] / Julio Chu ... [et al.].
Publication
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.

Details

Additional Authors
  • Chu, Julio.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Description
1 v.
Series Statement
NASA technical memorandum ; 4189
Subject
  • Low temperature research
  • Transonic wind tunnels
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 93-0047-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:4189
OCLC
marcive27838666
Title
High Reynolds number test of the Boeing TR77 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel [microform] / Julio Chu ... [et al.].
Imprint
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
Series
NASA technical memorandum ; 4189
Reproduction
Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1992. 1 microfiche.
Added Author
Chu, Julio.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:4189
Research Call Number
READEX Microfiche NAS 1.15:4189
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