Wind tunnel tests on an airfoil equipped with a split flap and a slot /

Wind tunnel tests on an airfoil equipped with a split flap and a slot /

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Bibliographic Details
Author / Creator:	Bamber, M. J., author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929.
Description:	1 online resource (6 pages, 5 unnumbered pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 324 Technical note (United States. National Advisory Committee for Aeronautics) ; 324.
Subject:	Aerofoils. Flaps (Airplanes) Wind tunnel testing. Lift (Aerodynamics) -- Measurement. Aerofoils. Flaps (Airplanes) Wind tunnel testing.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12553703

Hidden Bibliographic Details
Other authors / contributors:	United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"October, 1929." No Federal Depository Library Program (FDLP) item number. Includes bibliographical reference (page 5). Description based on online resource, PDF version; title from title page (TRAIL, viewed August 31, 2020).
Other form:	Print version: Bamber, Millard J. Wind tunnel tests on an airfoil equipped with a split flap and a slot
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/324

Description
Item Description:	"October, 1929." No Federal Depository Library Program (FDLP) item number.
Physical Description:	1 online resource (6 pages, 5 unnumbered pages) : illustrations.
Bibliography:	Includes bibliographical reference (page 5).