Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow /

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Bibliographic Details
Author / Creator:Hallissy, James B.
Imprint:[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1989.
Description:225 pages : illustrations ; 28 cm.
Language:English
Series:NASA technical memorandum ; 4124
NASA technical memorandum ; 4124.
Subject:Wind tunnels.
Airplanes -- Wings.
Laminar flow.
Aircraft configurations.
Laminar flow.
Pressure distribution.
Variable sweep wings.
Wind tunnel tests.
Wing loading.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/7242528
Hidden Bibliographic Details
Other authors / contributors:Phillips, Pamela S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Notes:"August 1989."
"National Aeronautics and Space Administration Cod NTT-4."
Includes bibliographical references (pages 5-6).
Available via Internet from the NASA Technical Report Server web site. Address as of 7/10/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890017439%5F1989017439.pdf; current access available via PURL.
GPO item no.:0830-D (MF)
0830-D (online)
Govt.docs classification:NAS 1.15:4124