Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base /

Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base /

Saved in:
Bibliographic Details
Author / Creator:Love, Eugene S., author.
Imprint:Washington, [D.C.] : National Advisory Committee for Aeronautics, 1956.
Description:1 online resource (62 pages) : illustrations.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 3709
Technical note (United States. National Advisory Committee for Aeronautics) ; 3709.
Subject:
Aerodynamic load.
Aerodynamics, Supersonic.
Body of revolution.
Aerodynamic load.
Aerodynamics, Supersonic.
Body of revolution.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12381222
Hidden Bibliographic Details
Other authors / contributors:United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"September 1956."
"Supersedes recently declassified NACA Research Memorandum L9K09 by Eugene S. Love, 1950"--Page 1.
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical references (pages 25-26).
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 13, 2020).
Other form:Print version: Love, Eugene S., Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/3709

Similar Items