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Feasibility and benefits of laminar flow control on supersonic cruise airplanes / A.G. Powell, S. Agrawal, T.R. Lacey.

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Format:
Book
Government document
Author/Creator:
Powell, A. G.
Contributor:
Agrawal, S.
Lacey, T. R.
Langley Research Center
Series:
NASA contractor report ; NASA CR-181817.
NASA contractor report ; 181817
Language:
English
Subjects (All):
Boundary layer control.
Laminar boundary layer.
Laminar flow.
Physical Description:
1 online resource (1 volume)
Place of Publication:
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
Notes:
Title from title screen (viewed June 9, 2009).
Other Format:
Powell, A.G. Feasibility and benefits of laminar flow control on supersonic cruise airplanes.
OCLC:
384172382

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