Feasibility and benefits of laminar flow control on supersonic cruise airplanes /

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Bibliographic Details
Author / Creator:Powell, A. G.
Imprint:Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
Description:1 volume.
Language:English
Series:NASA contractor report ; 181817
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.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12694830
Hidden Bibliographic Details
Other authors / contributors:Agrawal, Sudhir.
Lacey, T. R.
Langley Research Center.
Notes: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.
Other form:Powell, A. G. Feasibility and benefits of laminar flow control on supersonic cruise airplanes. 1 v.
GPO item no.:0830-H-14 (MF)
0830-H-14 (online)
Govt.docs classification:NAS 1.26:181817