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Title	Pressure distribution over a Clark Y-H airfoil section with a split flap /
Format	online resource
Internet Access	https://purl.fdlp.gov/GPO/gpo159327
Author	Wenzinger, Carl J. (Carl Joseph), 1903-1988, author.
Published	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1937.

SuDoc Number	Y 3.N 21/5:6/627
Description	1 online resource (5 pages, 6 unnumbered pages) : illustrations.
Content Type	text
Series	(Technical note (United States. National Advisory Committee for Aeronautics) ; 627.)
General Note	"December 1937."
	No Federal Depository Library Program (FDLP) item number.
Bibliography	Includes bibliographical references (page 5).
Metadata Source	Description based on online resource, PDF version; title from title page (TRAIL, viewed August 30, 2021).
Subject - LC	Aerofoils.
	Split flaps (Airplanes)
	Aerodynamic load.
	Wind tunnel testing.
Added Entry	United States. National Advisory Committee for Aeronautics, issuing body.
Linking Field	Print version: Wenzinger, Carl J. Pressure distribution over a Clark Y-H airfoil section with a split flap (OCoLC)645501223
URL	Address at time of PURL creation https://digital.library.unt.edu/ark:/67531/metadc54417/m2/1/high_res_d/19930081439.pdf

Holdings	All items

OCLC Number	(OCoLC)1159597638
CGP Record Link	https://catalog.gpo.gov:443/F/?func=direct&doc_number=001163295&local_base=GPO01PUB
System Number	001163295