Effect of aerofoil aspect ratio on the slope of the lift curve /

Effect of aerofoil aspect ratio on the slope of the lift curve /

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Bibliographic Details
Author / Creator:Diehl, Walter S. (Walter Stuart), 1893-1976, author.
Imprint:[Washington, D.C.] : National Advisory Committee for Aeronautics, 1922.
Description:1 online resource (4 pages, 1 unnumbered page) : illustration.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 79
Technical note (United States. National Advisory Committee for Aeronautics) ; 79.
Subject:
Aerofoils.
Aerofoils -- Mathematical models.
Aspect ratio (Aerofoils)
Lift (Aerodynamics)
Aerofoils.
Aerofoils -- Mathematical models.
Aspect ratio (Aerofoils)
Lift (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12091916
Hidden Bibliographic Details
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"January, 1922."
No Federal Depository Library Program (FDLP) item number.
Description based on online resource, PDF version; title from title page (TRAIL, viewed February 7, 2020).
Other form:Print version: Diehl, Walter S. Effect of aerofoil aspect ratio on the slope of the lift curve
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/79

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