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Title	Effect of air-entry angle on performance of a 2-stroke-cycle compression-ignition engine /
Format	online resource
Internet Access	https://purl.fdlp.gov/GPO/gpo158500
Author	Earle, Sherod L., author.
Published	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1937.

SuDoc Number	Y 3.N 21/5:6/610
Description	1 online resource (13 pages, 13 unnumbered pages) : illustrations.
Content Type	text
Series	(Technical note (United States. National Advisory Committee for Aeronautics) ; 610.)
General Note	"August 1937."
	No Federal Depository Library Program (FDLP) item number.
Bibliography	Includes bibliographical references (page 13).
Metadata Source	Description based on online resource, PDF version; title from title page (TRAIL, viewed August 4, 2021).
Subject - LC	Airplanes -- Motors.
	Aircraft gas-turbines -- Combustion chambers.
	Two-stroke cycle engines.
	Aeronautics -- Research.
Added Entry	Dutee, Francis J., author.
Added Entry	United States. National Advisory Committee for Aeronautics, issuing body.
Linking Field	Print version: Earle, Sherod L. Effect of air-entry angle on performance of a 2-stroke-cycle compression-ignition engine (OCoLC)62146097
URL	Address at time of PURL creation https://digital.library.unt.edu/ark:/67531/metadc54346/m2/1/high_res_d/19930081402.pdf

Holdings	All items

OCLC Number	(OCoLC)1159597614
CGP Record Link	https://catalog.gpo.gov:443/F/?func=direct&doc_number=001162998&local_base=GPO01PUB
System Number	001162998