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Title	Wind tunnel pressure distribution tests on an airfoil with trailing edge flap /
Format	online resource
Internet Access	https://purl.fdlp.gov/GPO/gpo144235
Author	Wenzinger, Carl J. (Carl Joseph), 1903-1988, author.
Published	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929.

SuDoc Number	Y 3.N 21/5:6/326
Description	1 online resource (10 pages, 12 unnumbered pages) : illustrations.
Content Type	text
Series	(Technical note (United States. National Advisory Committee for Aeronautics) ; 326.)
General Note	"October, 1929."
	No Federal Depository Library Program (FDLP) item number.
Bibliography	Includes bibliographical references (pages 7-8).
Metadata Source	Description based on online resource, PDF version; title from title page (TRAIL, viewed August 31, 2020).
Subject - LC	Aerofoils.
	Flaps (Airplanes)
	Wind tunnel testing.
	Aerodynamic load -- Testing.
Added Entry	Loeser, Oscar Jr., author.
Added Entry	United States. National Advisory Committee for Aeronautics, issuing body.
Linking Field	Print version: Wenzinger, Carl J. Wind tunnel pressure distribution tests on an airfoil with trailing edge flap (OCoLC)642704145
URL	Address at time of PURL creation https://digital.library.unt.edu/ark:/67531/metadc53999/m2/1/high_res_d/19930081109.pdf

Holdings	All items

OCLC Number	(OCoLC)1136490256
CGP Record Link	https://catalog.gpo.gov:443/F/?func=direct&doc_number=001128983&local_base=GPO01PUB
System Number	001128983