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Title	Fuselage-drag tests in the variable-density wind tunnel : streamline bodies of revolution, fineness ratio of 5 /
Format	online resource
Internet Access	https://purl.fdlp.gov/GPO/gpo158610
Author	Abbott, Ira H. A., author.
Published	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1937.

SuDoc Number	Y 3.N 21/5:6/614
Variation of Title	Streamline bodies of revolution, fineness ratio of 5
Description	1 online resource (11 pages, 5 unnumbered pages) : illustrations.
Content Type	text
Series	(Technical note (United States. National Advisory Committee for Aeronautics) ; 614.)
General Note	"September 1937."
	No Federal Depository Library Program (FDLP) item number.
Bibliography	Includes bibliographical references (page 8).
Metadata Source	Description based on online resource, PDF version; title from title page (TRAIL, viewed August 6, 2021).
Subject - LC	Airplanes -- Fuselage.
	Drag (Aerodynamics)
	Wind tunnel testing.
Added Entry	United States. National Advisory Committee for Aeronautics, issuing body.
Linking Field	Print version: Abbott, Ira H. Fuselage-drag tests in the variable-density wind tunnel: streamline bodies of revolution, fineness ratio of 5 (OCoLC)645480263
URL	Address at time of PURL creation https://digital.library.unt.edu/ark:/67531/metadc54304/m2/1/high_res_d/19930081378.pdf

Holdings	All items

OCLC Number	(OCoLC)1159597625
CGP Record Link	https://catalog.gpo.gov:443/F/?func=direct&doc_number=001163169&local_base=GPO01PUB
System Number	001163169