Real-time simulation of supersonic inletsA previously published real-time simulation algorithm, the matrix stability region placement (MSRP) method, is used to simulate a small perturbation model of the NASA Lewis Mach 2.5 40-60 mixed compression inlet. The model is representative of high-speed internal flow propulsion systems which can be approximated as quasi-one-dimensional flows. The resulting system of equations, which is stiff, is also simulated by the second-order Adam-Bashforth method. It is shown that the MSRP method can be used to simulate small perturbation models of high-speed internal flow propulsion systems in real time.
Document ID
19910066367
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mossayebi, F. (Akron Univ. Akron, OH, United States)
Hartley, T. T. (Akron Univ. Akron, OH, United States)
De Abreu-Garcia, J. A. (Akron, University OH, United States)
Pansino, S. R. (Youngstown State University OH, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aerodynamics
Meeting Information
Meeting: IEEE International Conference on Systems Engineering