Cover Image

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

Bibliographic Details
Main Author: Hallissy, James B.
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors: Phillips, Pamela S.
Format: Government Document Microform Book
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1989.
Series:NASA technical memorandum ; 4124.
Subjects:
Wind tunnels.
Airplanes > Wings.
Laminar flow.
Aircraft configurations.
Pressure distribution.
Variable sweep wings.
Wind tunnel tests.
Wing loading.
Online Access:https://purl.fdlp.gov/GPO/LPS96586
Description
Item Description:"August 1989."
"National Aeronautics and Space Administration Cod NTT-4."
Microform.
Physical Description:225 pages : illustrations ; 28 cm.
Also 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_1989017439.pdf; current access available via PURL.
Bibliography:Includes bibliographical references (pages 5-6).