Application of laminar flow control to supersonic transport configurations.

Saved in:
Bibliographic Details
Imprint:Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
Description:1 volume.
Language:English
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.
Wings.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12670274
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: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900016628%5F1990016628.pdf; current access is available via PURL.
GPO item no.:0830-H-14 (MF)
0830-H-14 (online)
Govt.docs classification:NAS 1.26:181917