Wind tunnel pressure distribution tests on a series of biplane wing models. Part I. Effects of changes in stagger and gap /

Saved in:

Bibliographic Details
Author / Creator:	Knight, Montgomery, author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929.
Description:	1 online resource (13 pages, 20 unnumbered pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 310 Technical note (United States. National Advisory Committee for Aeronautics) ; 310.
Subject:	Airplanes -- Wings -- Design and construction. Wind tunnel testing. Biplanes. Airplanes -- Wings -- Design and construction. Wind tunnel testing.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12381246

Hidden Bibliographic Details
Varying Form of Title:	Effects of changes in stagger and gap
Other authors / contributors:	Noyes, Richard W., author. United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"July, 1929." 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 August 18, 2020).
Other form:	Print version: Knight, Montgomery. Wind tunnel pressure distribution tests on a series of biplane wing models
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/310

Similar Items