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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