Analysis of available data on the effects of tabs on control-surface hinge moments /

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Bibliographic Details
Author / Creator:Crandall, Stewart M., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1946.
Description:1 online resource (28 pages, 14 unnumbered pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 1049
Technical note (United States. National Advisory Committee for Aeronautics) ; 1049.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12346613
Hidden Bibliographic Details
Other authors / contributors:Murray, Harry E., author.
United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"May 1946."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (pages 23-25).
Description based on online resource, PDF version; title from title page (TRAIL, viewed July 7, 2020).
Other form:Print version: Crandall, Stewart M., Analysis of available data on the effects of tabs on control-surface hinge moments
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/1049

MARC

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490 1 |a Technical notes / National Advisory Committee for Aeronautics ;  |v No. 1049 
588 |a Description based on online resource, PDF version; title from title page (TRAIL, viewed July 7, 2020). 
500 |a "May 1946." 
500 |a No Federal Depository Library Program (FDLP) item number. 
504 |a Includes bibliographical references (pages 23-25). 
650 0 |a Airplanes  |x Control surfaces.  |0 http://id.loc.gov/authorities/subjects/sh85002798 
650 0 |a Hinge moments (Aerodynamics)  |0 http://id.loc.gov/authorities/subjects/sh85060958 
650 0 |a Tabs (Airplanes)  |0 http://id.loc.gov/authorities/subjects/sh85131827 
650 0 |a Flaps (Airplanes)  |0 http://id.loc.gov/authorities/subjects/sh85049001 
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650 7 |a Hinge moments (Aerodynamics)  |2 fast  |0 (OCoLC)fst00957213 
650 7 |a Tabs (Airplanes)  |2 fast  |0 (OCoLC)fst01141800 
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