Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. X. Various control devices on a wing with a fixed auxiliary airfoil /

Saved in:

Bibliographic Details
Author / Creator:	Weick, Fred E., author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1933.
Description:	1 online resource (18 pages, 9 unnumbered pages) : illustrations.
Language:	English
Series:	Technical note / National Advisory Committee for Aeronautics ; No. 451 Technical note (United States. National Advisory Committee for Aeronautics) ; 451.
Subject:	Airplanes -- Wings -- Testing. Airplanes -- Control surfaces. Spoilers (Airplanes) Wind tunnel testing. Airplanes -- Control surfaces. Airplanes -- Wings -- Testing. Spoilers (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/12695145

Hidden Bibliographic Details
Varying Form of Title:	Various control devices on a wing with a fixed auxiliary airfoil
Other authors / contributors:	Noyes, Richard W., author. United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"March, 1933." No Federal Depository Library Program (FDLP) item number. Includes bibliographical references (pages 15-16). Description based on online resource, PDF version; title from title page (TRAIL, viewed January 11, 2021).
Other form:	Print version: Weick, Fred E. Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. X. Various control devices on a wing with a fixed auxiliary airfoil
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/451

Similar Items