The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 /

The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 /

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Bibliographic Details
Author / Creator:	Burbank, Paige B., author.
Imprint:	Washington, [D.C.] : National Advisory Committee for Aeronautics, 1953.
Description:	1 online resource (37 pages) : illustrations.
Language:	English
Series:	Technical notes / National Advisory Committee for Aeronautics ; No. 2921 Technical note (United States. National Advisory Committee for Aeronautics) ; 2921.
Subject:	Nozzles -- Fluid dynamics. Mach number. Supersonic nozzles -- Design and construction. Mach number. Nozzles -- Fluid dynamics. Supersonic nozzles -- Design and construction.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12381211

Hidden Bibliographic Details
Other authors / contributors:	Byrne, Robert W., author. United States. National Advisory Committee for Aeronautics, issuing body.
Notes:	"April 1953." No Federal Depository Library Program (FDLP) item number. Includes bibliographical references (page 11). Description based on online resource, PDF version; title from title page (TRAIL, viewed July 31, 2020).
Other form:	Print version: Burbank, Paige B., Aerodynamic design and calibration of an asymmetric variable Mach number nozzle with sliding block for the Mach number range 1.27 to 2.75
GPO item no.:	9999 (online)
Govt.docs classification:	Y 3.N 21/5:6/2921

Description
Item Description:	"April 1953." No Federal Depository Library Program (FDLP) item number.
Physical Description:	1 online resource (37 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 11).