Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system /

Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system /

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Bibliographic Details
Main Authors:	Maddalon, Dal V, Maddalon, Dal V. (Author), Braslow, Albert L. (Author)
Corporate Authors:	United States National Aeronautics and Space Administration. Scientific and Technical Information Division, Langley Research Center
Other Authors:	Braslow, Albert L
Format:	Government Document Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990 [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, March 1990
Series:	NASA technical paper ; 2966 NASA technical paper 2966
Subjects:	Airplanes > Flight testing Laminar flow Airplanes > Control systems Boundary layer control Flight simulation Flight tests Leading edges
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Stanford University

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Call Number:	ISIL:US-CST NAS 1.15:2966