The effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests /

The effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests /

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Bibliographic Details
Author / Creator:Weick, Fred E., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929.
Description:1 online resource (22 pages, 23 unnumbered pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 322
Technical note (United States. National Advisory Committee for Aeronautics) ; 322.
Subject:
Airplanes -- Wings.
Airplanes -- Motors.
Drag (Aerodynamics)
Wind tunnel testing.
Airplanes -- Motors.
Airplanes -- Wings.
Drag (Aerodynamics)
Wind tunnel testing.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12553702
Hidden Bibliographic Details
Other authors / contributors:Wood, Donald H, author.
United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"October, 1929."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 6).
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 19, 2020).
Other form:Print version: Weick, Fred E. Effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/322

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