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Feasibility and benefits of laminar flow control on supersonic cruise airplanes

Author: A G Powell; S Agrawal; T R Lacey; Langley Research Center.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
Series: NASA contractor report, NASA CR-181817.
Edition/Format:   eBook : Document : National government publication : EnglishView all editions and formats
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Additional Physical Format: Powell, A.G.
Feasibility and benefits of laminar flow control on supersonic cruise airplanes.
1 v.
(OCoLC)384139602
Material Type: Document, Government publication, National government publication, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: A G Powell; S Agrawal; T R Lacey; Langley Research Center.
OCLC Number: 384172382
Notes: Title from title screen (viewed Jun. 9, 2009).
Description: 1 volume.
Details: 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_1989017470.pdf ; current access is available via PURL.
Series Title: NASA contractor report, NASA CR-181817.
Responsibility: A.G. Powell, S. Agrawal, T.R. Lacey.

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