Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10⁶ to 11.0 x 10⁶ /

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Bibliographic Details
Author / Creator:	Schaefer, Raymond F., author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1949.
Description:	1 online resource (12 pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 1998 Technical note (United States. National Advisory Committee for Aeronautics) ; 1998.
Subject:	Aerofoils. Aerodynamics. Lift (Aerodynamics) Drag (Aerodynamics) Pitching (Aerodynamics) Wind tunnel testing. Aerodynamics. Aerofoils. Drag (Aerodynamics) Lift (Aerodynamics) Pitching (Aerodynamics) Wind tunnel testing.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12346604

Hidden Bibliographic Details
Varying Form of Title:	Aerodynamic characteristics of the National Advisory Committee for Aeronautics 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6)
Other authors / contributors:	Smith, Hamilton A., author. United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"December 1949." 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 July 9, 2020).
Other form:	Paper version: Schaefer, Raymond F., Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6)
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/1998

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