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Title	The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear /
Format	online resource
Internet Access	https://purl.fdlp.gov/GPO/gpo139591
Author	Weick, Fred E., author.
Published	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1932.

SuDoc Number	Y 3.N 21/5:6/422
Description	1 online resource (7 pages, 11 unnumbered pages) : illustrations.
Content Type	text
Series	(Technical note (United States. National Advisory Committee for Aeronautics) ; 422.)
General Note	"May, 1932."
	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 June 11, 2020).
Subject - LC	Wind tunnel testing.
	Split flaps (Airplanes)
	Airplanes -- Models -- Wings.
	Trailing edge flaps.
Added Entry	Harris, Thomas A., author.
Added Entry	United States. National Advisory Committee for Aeronautics, issuing body.
Linking Field	Print version: Weick, Fred A., The Aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear (OCoLC)643508269
URL	Address at time of PURL creation https://digital.library.unt.edu/ark:/67531/metadc54116/m2/1/high_res_d/19930081228.pdf

Holdings	All items

OCLC Number	(OCoLC)1100474465
CGP Record Link	https://catalog.gpo.gov:443/F/?func=direct&doc_number=001124341&local_base=GPO01PUB
System Number	001124341