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

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Bibliographic Details
Author / Creator:Maddalon, Dal V., author.
Imprint:[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, March 1990.
Description:1 online resource (38 pages) : illustrations.
Language:English
Series:NASA technical paper ; 2966
NASA technical paper ; 2966.
Subject:Boundary layer control.
Laminar flow.
Leading edges.
Flight simulation.
Flight tests.
Airplanes -- Control systems.
Laminar flow.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10964110
Hidden Bibliographic Details
Other authors / contributors:Braslow, Albert L., author.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (1987-1990 ), issuing body.
Notes:"March 1990"--Report documentation page.
"Performing organization: NASA Langley Research Center"--Report documentation page.
Includes bibliographical references (page 9).
Technical paper.
National Aeronautics and Space Administration 505-60-41-01
L-16589
Description based on online resource; title from PDF title page (NASA, viewed Jan. 24, 2017).
Other form:Print version: Maddalon, Dal V. Simulated-airline-service flight tests of laminar flow control with perforated-surface suction system
Microfiche version: Maddalon, Dal V. Simulated-airline-service flight tests of laminar-flow control with perforated-surface suction system
GPO item no.:0830-H-15 (online)
Govt.docs classification:NAS 1.60:2966