The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals /

The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals /

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Bibliographic Details
Author / Creator:Munk, Max M. (Max Michael), 1890- author.
Imprint:[Washington, D.C.] : National Advisory Committee for Aeronautics, 1923.
Description:1 online resource (9 pages, 2 unnumbered pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 122
Technical note (United States. National Advisory Committee for Aeronautics) ; 122.
Subject:Lift (Aerodynamics)
Angle of attack (Aerodynamics)
Aerofoils.
Camber (Aerofoils)
Aerofoils.
Angle of attack (Aerodynamics)
Camber (Aerofoils)
Lift (Aerodynamics)
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12285007
Hidden Bibliographic Details
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"January, 1923."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 1).
Description based on online resource, PDF version; title from title page (TRAIL, viewed March 26, 2020).
Other form:Print version: Munk, Max M. Determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/122

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