Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° /

Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° /

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Bibliographic Details
Author / Creator:Penland, Jim A., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1957.
Description:1 online resource (32 pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 3861
Technical note (United States. National Advisory Committee for Aeronautics) ; 3861.
Subject:
Cylinders -- Aerodynamics.
Aerodynamic load.
Wind tunnel testing.
Hypersonic wind tunnels.
Aerodynamic load.
Cylinders -- Aerodynamics.
Hypersonic wind tunnels.
Wind tunnel testing.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12381204
Hidden Bibliographic Details
Varying Form of Title:Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to ninety degrees
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"January 1957."
"Supersedes recently declassified NACA Research Memorandum L54A14 by Jim A. Penland, 1954"--Page 1.
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (page 13-14).
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 13, 2020).
Other form:Print version: Penland, Jim A., Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90 degrees
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/3861

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