Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) /

Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) /

Saved in:
Bibliographic Details
Author / Creator:Heald, R. H., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1933.
Description:1 online resource (12 pages, 3 unnumbered pages) : illustrations.
Language:English
Series:Technical note / National Advisory Committee for Aeronautics ; No. 441
Technical note (United States. National Advisory Committee for Aeronautics) ; 441.
Subject:
Ailerons.
Flaps (Airplanes)
Rolling (Aerodynamics)
Yawing (Aerodynamics)
Hinge moments (Aerodynamics)
Wind tunnel testing.
Hinge moments (Aerodynamics)
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/12695150
Hidden Bibliographic Details
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"January, 1933."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 12).
Description based on online resource, PDF version; title from title page (TRAIL, viewed January 8, 2021).
Other form:Print version: Heald, R. H. Rolling, yawing, and hinge moments produced by rectangular ailerons
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/441

Similar Items