Wind tunnel pressure distribution tests on an airfoil with trailing edge flap /

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Bibliographic Details
Author / Creator:	Wenzinger, Carl J. (Carl Joseph), 1903-1988, author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929.
Description:	1 online resource (10 pages, 12 unnumbered pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 326 Technical note (United States. National Advisory Committee for Aeronautics) ; 326.
Subject:	Aerofoils. Flaps (Airplanes) Wind tunnel testing. Aerodynamic load -- Testing. Aerodynamic load -- Testing. Wind tunnel testing.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12553696

Hidden Bibliographic Details
Other authors / contributors:	Loeser, Oscar, author. United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"October, 1929." No Federal Depository Library Program (FDLP) item number. Includes bibliographical references (pages 7-8). Description based on online resource, PDF version; title from title page (TRAIL, viewed August 31, 2020).
Other form:	Print version: Wenzinger, Carl J. Wind tunnel pressure distribution tests on an airfoil with trailing edge flap
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/326

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