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

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Bibliographic Details
Main Author: Powell, A. G.
Corporate Author: Langley Research Center
Other Authors: Agrawal, S., Lacey, T. R.
Format: Government Document Book
Language:English
Published: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
Series:NASA contractor report ; NASA CR-181817.
Subjects:
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.
Online Access:https://purl.fdlp.gov/GPO/LPS113610
Description
Item Description:Title from title screen (viewed Jun. 9, 2009).
Electronic resource.
Physical Description:1 volume
Format:Mode of access: 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.