Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section /

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Bibliographic Details
Author / Creator:	Smith, Hamilton A., author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1950.
Description:	1 online resource (18 pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 2074 Technical note (United States. National Advisory Committee for Aeronautics) ; 2074.
Subject:	Aerofoils. Aerodynamics. Lift (Aerodynamics) Drag (Aerodynamics) Pitching (Aerodynamics) Reynolds number. Aerodynamics. Aerofoils. Drag (Aerodynamics) Lift (Aerodynamics) Pitching (Aerodynamics) Reynolds number.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12346599

Hidden Bibliographic Details
Varying Form of Title:	Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the National Advisory Committee for Aeronautics 0012 airfoil section
Other authors / contributors:	Schaefer, Raymond F., author. United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"April 1950." No Federal Depository Library Program (FDLP) item number. Includes bibliographical references (page 9). Description based on online resource, PDF version; title from title page (TRAIL, viewed July 15, 2020).
Other form:	Paper version: Smith, Hamilton A., Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/2074

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