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Transonic and Supersonic Inviscid Flow Equations in 3-D Eccentric Nozzles

[+] Author Affiliations
Ali Reza Mazaheri, Goodarz Ahmadi

Clarkson University, Potsdam, NY

Homayoon Emdad

Shiraz University, Shiraz, Iran

Paper No. FEDSM2002-31092, pp. 1225-1230; 6 pages
doi:10.1115/FEDSM2002-31092
From:
  • ASME 2002 Joint U.S.-European Fluids Engineering Division Conference
  • Volume 2: Symposia and General Papers, Parts A and B
  • Montreal, Quebec, Canada, July 14–18, 2002
  • Conference Sponsors: Fluids Engineering Division
  • ISBN: 0-7918-3616-9 | eISBN: 0-7918-3600-2
  • Copyright © 2002 by ASME

abstract

Three dimensional unsteady inviscid flows in convergent-divergent nozzles is of importance in understanding the stability of rockets and jet propulsion. A computer program for evaluating unsteady inviscid flow conditions in three-dimensional eccentric as well as concentric nozzles is developed. The program uses the cell-centered finite-volume method based on Roe’s approximate Riemann solver scheme. The flow simulation results in concentric circular nozzles are compared with the one-dimensional analytic solutions and the accuracy of the computation model is verified. The results for steady and unsteady flows through eccentric and concentric convergent-divergent nozzles are then presented. A range of exit to throat areas, pressure ratios, and inlet Mach number are considered.

Copyright © 2002 by ASME

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