Research Catalog

Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration

Title
Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [et al.].
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]

Details

Additional Authors
  • Campbell, Bryan A.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA/TM ; 1999-209701
Uniform Title
NASA technical memorandum ; 209701.
Alternative Title
Subsonic investigation of leading edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration
Subject
  • Subsonic wind tunnels
  • Leading edge flaps
  • Vortices
  • Supersonic transports
  • Aerodynamic configurations
  • Separated flow
Note
  • Shipping list no.: 2000-0596-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:209701
OCLC
marcive44120738
Title
Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [et al.].
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
Series
NASA/TM ; 1999-209701
NASA technical memorandum ; 209701.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000] 2 microfiches.
Added Author
Campbell, Bryan A.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:209701
Research Call Number
READEX Microfiche NAS 1.15:209701
View in Legacy Catalog