Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model /

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Bibliographic Details
Author / Creator:	Bamber, Millard J., author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1934.
Description:	1 online resource (8 pages, 5 unnumbered pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 515 Technical note (United States. National Advisory Committee for Aeronautics) ; 515.
Subject:	Aerodynamics. Spin (Aerodynamics) Split flaps (Airplanes) Wind tunnel testing. Aerodynamics. Spin (Aerodynamics) Split flaps (Airplanes) Wind tunnel testing.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12321602

Hidden Bibliographic Details
Other authors / contributors:	United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"December 1934" No Federal Depository Library Program (FDLP) item number Includes bibliographical references (page 8) Description based on online resource, PDF version; title from title page (TRAIL, viewed June 15, 2020)
Other form:	Print version: Bamber, Milard J., Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/515

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