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

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