Research Catalog

Results for the hybrid laminar flow control experiment conducted in the NASA Langley 3-FT transonic pressure tunnel on a 7-ft chord model

Title
Results for the hybrid laminar flow control experiment conducted in the NASA Langley 3-FT transonic pressure tunnel on a 7-ft chord model [microform] / Percy J. Bobbitt ... [et al.].
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]

Details

Additional Authors
  • Bobbitt, Percy J.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 107582
Subject
  • Aerofoils
  • Laminar flow
  • Transonic wind tunnels
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 94-0809-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:107582
OCLC
marcive31768240
Title
Results for the hybrid laminar flow control experiment conducted in the NASA Langley 3-FT transonic pressure tunnel on a 7-ft chord model [microform] / Percy J. Bobbitt ... [et al.].
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
Series
NASA technical memorandum ; 107582
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.
Added Author
Bobbitt, Percy J.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:107582
Research Call Number
READEX Microfiche NAS 1.15:107582
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