The effect of wing tip floating ailerons on the autorotation of a monoplane wing model /

The effect of wing tip floating ailerons on the autorotation of a monoplane wing model /

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Bibliographic Details
Author / Creator:Knight, Montgomery, author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1930.
Description:1 online resource (19 pages, 6 unnumbered pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 336
Technical note (United States. National Advisory Committee for Aeronautics) ; 336.
Subject:
Ailerons.
Flaps (Airplanes)
Rolling (Aerodynamics)
Wind tunnel testing.
Rolling (Aerodynamics)
Wind tunnel testing.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12670552
Hidden Bibliographic Details
Other authors / contributors:Wenzinger, Carl J. (Carl Joseph), 1903-1988, author.
United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"March, 1930."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 13).
Description based on online resource, PDF version; title from title page (TRAIL, viewed September 3, 2020).
Other form:Print version: Knight, Montgomery Effect of wing tip floating ailerons on the autorotation of a monoplane wing model
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/336

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