Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil /

Saved in:
Bibliographic Details
Author / Creator:Hahne, David E. (David Edgar)
Imprint:[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Description:48 pages : illustrations ; 28 cm.
Series:NASA technical paper ; 3133
NASA technical paper ; 3133.
Subject:Aerofoils -- Testing.
Airplanes -- Wings -- Testing.
Laminar flow.
Airfoil profiles.
Full scale tests.
Jet aircraft.
Laminar flow airfoils.
Low speed.
Semispan models.
Wind tunnel tests.
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6508772
Hidden Bibliographic Details
Other authors / contributors:Jordan, Frank L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Langley Research Center.
Notes:"September 1991."
Prepared at Langley Research Center.
Bibliography: pages 6-7.
Available via Internet from the NTRS web site. Address as of 3/16/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910020784%5F1991020784.pdf; current access is available via PURL.
GPO item no.:0830-H-15 (MF)
0830-H-15 (online)
Govt.docs classification:NAS 1.60:3133