Method of designing symmetrical flexible wall nozzle for continuous variation of Mach Number, developed by using small wall curvatures in lower Mach Number region and by applying K.FOELSCH theory for higher Mach Number (2.50).
Design and calibration of variable Mach Number nozzle
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 22 , n 7
1955
7 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Optimization design of variable Mach number wind tunnel nozzle by rotating profile
Online Contents | 2014
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