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A finite-difference solution for unsteady wave interactions with an application to the expansion tubeAn analytical study of the unsteady wave interaction of a shock wave overtaking a previously initiated shock tube flow has been conducted for a real gas by solving a finite-difference representation of the one-dimensional Navier-Stokes equations. This analysis has been used to determine the effect on the available test time of opening the secondary diaphragm in the expansion-tube operating cycle prior to the arrival of the incident shock wave. Special emphasis is placed on determining expansion-tube test-time limitations resulting from a nonuniform entropy distribution occurring during the early test-gas flow due to the varying Mach number of the incident shock wave as it traverses the expansion fan caused by the preopening process. Time distributions of velocity, temperature, pressure, and entropy at various distances from the diaphragm are presented as a function of the time required to open the diaphragm.
Document ID
19740033670
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Weilmuenster, K. J.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Fluid Mechanics
Meeting Information
Meeting: International Symposium on Recent Developments in Shock Tube Research
Location: Stanford, CA
Start Date: July 16, 1973
End Date: July 19, 1973
Accession Number
74A16420
Distribution Limits
Public
Copyright
Other

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