Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance /

Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance /

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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, 3 unnumbered pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 493 Technical note (United States. National Advisory Committee for Aeronautics) ; 493.
Subject:	Ailerons. Airplanes -- Wings. Rolling (Aerodynamics) Wind tunnel testing. Yawing (Aerodynamics) Ailerons. Airplanes -- Wings. Rolling (Aerodynamics) Wind tunnel testing. Yawing (Aerodynamics)
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12321605

Hidden Bibliographic Details
Other authors / contributors:	United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"March 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 12, 2020)
Other form:	Print version: Bamber, Millard J., Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/493

Description
Item Description:	"March 1934" No Federal Depository Library Program (FDLP) item number
Physical Description:	1 online resource (8 pages, 3 unnumbered pages) : illustrations.
Bibliography:	Includes bibliographical references (page 8)