Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° /

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Bibliographic Details
Author / Creator:	McLemore, H. Clyde, author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1954.
Description:	1 online resource (62 pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 3228 Technical note (United States. National Advisory Committee for Aeronautics) ; 3228.
Subject:	Angle of attack (Aerodynamics) Mathematical analysis. Propellers, Aerial -- Testing. Wind tunnel testing. Angle of attack (Aerodynamics) Mathematical analysis. Propellers, Aerial -- Testing. Wind tunnel testing.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12381221

Hidden Bibliographic Details
Varying Form of Title:	Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 degrees to 180 degrees
Other authors / contributors:	Cannon, Michael D., author. United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"June 1954." No Federal Depository Library Program (FDLP) item number. Includes bibliographical references (page 15). Description based on online resource, PDF version; title from title page (TRAIL, viewed August 5, 2020).
Other form:	Print version: McLemore, H. Clyde, Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 to 180 degrees
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/3228

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