Research Catalog

Feasibility and benefits of laminar flow control on supersonic cruise airplanes

Title
Feasibility and benefits of laminar flow control on supersonic cruise airplanes [microform] / A.G. Powell, S. Agrawal, T. R. Lacey.
Author
Powell, A. G.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]

Available Online

http://purl.access.gpo.gov/GPO/LPS113610

Details

Additional Authors
  • Agrawal, S.
  • Lacey, T. R.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA contractor report ; 181817
Uniform Title
NASA contractor report ; NASA CR-181817.
Subject
  • Aerodynamic configurations
  • Boundary layer control
  • Boundary layer stability
  • Feasibility analysis
  • Fighter aircraft
  • Laminar boundary layer
  • Laminar flow
  • Supersonic aircraft
  • Supersonic cruise aircraft research
  • Supersonic transports
Additional Formats (note)
  • Also available via Internet from the NTRS web site. Address as of 06/09/09: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890017470%5F1989017470.pdf ; current access is available via PURL.
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.26:181817
OCLC
384139602
Author
Powell, A. G.
Title
Feasibility and benefits of laminar flow control on supersonic cruise airplanes [microform] / A.G. Powell, S. Agrawal, T. R. Lacey.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
Series
NASA contractor report ; 181817
NASA contractor report ; NASA CR-181817.
Additional Formats
Also available via Internet from the NTRS web site. Address as of 06/09/09: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890017470%5F1989017470.pdf ; current access is available via PURL.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1989. 2 microfiches.
Connect to:
http://purl.access.gpo.gov/GPO/LPS113610
Added Author
Agrawal, S.
Lacey, T. R.
Langley Research Center.
Other Form:
Powell, A. G. Feasibility and benefits of laminar flow control on supersonic cruise airplanes. 1 v. (OCoLC)384172382
Gpo Item No.
0830-H-14 (MF)
0830-H-14 (online)
Sudoc No.
NAS 1.26:181817
View in Legacy Catalog