Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 /

Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 /

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Bibliographic Details
Author / Creator:Turner, M. J., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1950.
Description:1 online resource (46 pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 2213
Technical note (United States. National Advisory Committee for Aeronautics) ; 2213.
Subject:
Aerofoils.
Flaps (Airplanes)
Lift (Aerodynamics)
Pitching (Aerodynamics)
Hinge moments (Aerodynamics)
Aerofoils.
Flaps (Airplanes)
Hinge moments (Aerodynamics)
Lift (Aerodynamics)
Pitching (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12678724
Hidden Bibliographic Details
Other authors / contributors:Rabinowitz, S., author.
United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"October 1950"
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 19).
Description based on online resource, PDF version; title from title page (TRAIL, viewed July 16, 2020).
Other form:Print version: Turner, M. J., Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/2213

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