Application of laminar flow control to supersonic transport configurations.

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Bibliographic Details
Imprint:Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
Description:1 volume.
Series:NASA contractor report ; 181917
NASA contractor report ; NASA CR-181917.
Subject:Aerodynamic drag.
Boundary layer control.
Boundary layer stability.
Laminar boundary layer.
Pressure distribution.
Supersonic transports.
Wing planforms.
Format: E-Resource Microform U.S. Federal Government Document Book
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Hidden Bibliographic Details
Other authors / contributors:Langley Research Center.
Notes:"Contract NAS1-15325."
"July 1990."
Includes bibliographical references.
Available via Internet from the NTRS web site. Address as of 6/14/05:; current access is available via PURL.
GPO item no.:0830-H-14 (MF)
0830-H-14 (online) classification:NAS 1.26:181917