The aerodynamic characteristics of three tapered airfoils tested in the variable density wind tunnel /

The aerodynamic characteristics of three tapered airfoils tested in the variable density wind tunnel /

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Bibliographic Details
Author / Creator:Anderson, Raymond F., author.
Imprint:Washington [D.C.] : National Advisory Committee for Aeronautics, 1931.
Description:1 online resource (12 pages, 10 unnumbered pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 367
Technical note (United States. National Advisory Committee for Aeronautics) ; no. 367.
Subject:
Wind tunnel testing.
Aerofoils.
Lift (Aerodynamics)
Drag (Aerodynamics)
Moments of inertia.
Drag (Aerodynamics)
Lift (Aerodynamics)
Moments of inertia.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12321419
Hidden Bibliographic Details
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"February, 1931."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 8).
Description based on online resource, PDF version; title from title page (TRAIL, viewed June 10, 2020).
Other form:Print version: Anderson, Raymond F. Aerodynamic characteristics of three tapered airfoils tested in the Variable Density Wind Tunnel
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/367

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