Aerodynamic tests of a low aspect ratio tapered wing with various flaps, for use on tailless airplanes /

Aerodynamic tests of a low aspect ratio tapered wing with various flaps, for use on tailless airplanes /

Saved in:
Bibliographic Details
Author / Creator:Weick, Fred E., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1933.
Description:1 online resource (6 pages, 6 unnumbered pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 463
Technical note (United States. National Advisory Committee for Aeronautics) ; 463.
Subject:
Airplanes, Tailless.
Aspect ratio (Aerofoils)
Flaps (Airplanes)
Wind tunnel testing.
Airplanes, Tailless.
Aspect ratio (Aerofoils)
Flaps (Airplanes)
Wind tunnel testing.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12553685
Hidden Bibliographic Details
Other authors / contributors:Sanders, Robert, 1908-1992, author.
United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"June 1933."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 6).
Description based on online resource, PDF version; title from title page (TRAIL, viewed June 12, 2020).
Other form:Print version: Weick, Fred E., Aerodynamic tests of a low aspect ratio tapered wing with various flaps, for use on tailless airplanes
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/463

Similar Items