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

Description
Item Description:	"October, 1929." No Federal Depository Library Program (FDLP) item number.
Physical Description:	1 online resource (22 pages, 23 unnumbered pages) : illustrations.
Bibliography:	Includes bibliographical references (page 6).