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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

Internet

https://purl.fdlp.gov/GPO/LPS96586

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Holdings details from Available Online
Call Number: NAS 1.15:4124
 
Call Number Status Get It
NAS 1.15:4124 Available

Evans: US Documents Microfiche (3rd floor)

Holdings details from Evans: US Documents Microfiche (3rd floor)
Call Number: NAS 1.15:4124
 
Call Number Status Get It
NAS 1.15:4124 Available