Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow /

Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow /

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Bibliographic Details
Author / Creator:Watkins, Charles E., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1951.
Description:1 online resource (44 pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 2457
Technical note (United States. National Advisory Committee for Aeronautics) ; 2457.
Subject:
Airplanes -- Wings, Swept-back.
Airplanes -- Wings, Triangular.
Leading edges (Aerodynamics)
Oscillating wings (Aerodynamics)
Airplanes -- Wings, Swept-back.
Airplanes -- Wings, Triangular.
Leading edges (Aerodynamics)
Oscillating wings (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12346621
Hidden Bibliographic Details
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"September 1951."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 34).
Description based on online resource, PDF version; title from title page (TRAIL, viewed July 16, 2020).
Other form:Print version: Watkins, Charles E., Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/2457

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