Wind tunnel pressure distribution tests on a series of biplane wing models. Part II. Effects of changes in decalage, dihedral, sweepback and overhang /

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Bibliographic Details
Author / Creator:	Knight, Montgomery, author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1929.
Description:	1 online resource (6 pages, 32 unnumbered pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 325 Technical note (United States. National Advisory Committee for Aeronautics) ; 325.
Subject:	Airplanes -- Dihedral wings. Airplanes -- Models -- Testing. Airplanes -- Wings, Swept-back. Aerodynamic load -- Testing. Wind tunnel testing. Biplanes. Aerodynamic load -- Testing. Airplanes -- Dihedral wings. Airplanes -- Models -- Testing. Airplanes -- Wings, Swept-back. Wind tunnel testing.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12553704

Hidden Bibliographic Details
Varying Form of Title:	Effects of changes in decalage, dihedral, sweepback and overhang
Other authors / contributors:	Noyes, Richard W., author. United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"October, 1929." Includes errata. No Federal Depository Library Program (FDLP) item number. Includes bibliographical reference (page 6). Description based on online resource, PDF version; title from title page (TRAIL, viewed August 31, 2020).
Other form:	Print version: Knight, Montgomery Wind tunnel pressure distribution tests on a series of biplane wing models. Part II, Effects of changes in decalage, dihedral, sweepback and overhang
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/325

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