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

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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