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Title	Wind tunnel pressure distribution tests on a series of biplane wing models. Part III, Effects of changes in various combinations of stagger, gap, sweepback, and decalage /
Format	online resource
Internet Access	https://purl.fdlp.gov/GPO/gpo144366
Author	Knight, Montgomery, author.
Published	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929.

SuDoc Number	Y 3.N 21/5:6/330
Variation of Title	Effects of changes in various combinations of stagger, gap, sweepback, and decalage
Description	1 online resource (6 pages, 22 unnumbered pages) : illustrations.
Content Type	text
Series	(Technical note (United States. National Advisory Committee for Aeronautics) ; 330.)
General Note	"December, 1929."
	Includes errata.
	No Federal Depository Library Program (FDLP) item number.
Bibliography	Includes bibliographical references (page 6).
Metadata Source	Description based on online resource, PDF version; title from title page (TRAIL, viewed September 2, 2020).
Subject - LC	Aerodynamic load -- Testing.
	Airplanes -- Models -- Testing.
	Airplanes -- Wings, Swept-back.
	Wind tunnel testing.
	Biplanes.
Added Entry	Noyes, Richard W., author.
Added Entry	United States. National Advisory Committee for Aeronautics, issuing body.
Linking Field	Print version: Knight, Montgomery Wind tunnel pressure distribution tests on a series of biplane wing models. Part III : Effects of changes in various combinations of stagger, gap, sweepback and decalage (OCoLC)642714170
URL	Address at time of PURL creation https://digital.library.unt.edu/ark:/67531/metadc54019/m2/1/high_res_d/19930081130.pdf

Holdings	All items

OCLC Number	(OCoLC)1136490288
CGP Record Link	https://catalog.gpo.gov:443/F/?func=direct&doc_number=001129254&local_base=GPO01PUB
System Number	001129254

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