Nonuniform nozzle flow effects on base pressure at supersonic flightspeeds
Author:
Affiliation:
1. University of Illinois at Urbana-Champaign, Urbana, Illinois
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9421
Reference19 articles.
1. MacCormack, R. W. "A Numerical Method for Solving the Equations of Compressible Viscous Flow,'* AIAA Journal, Vol.20, Sept. 1982, pp.1275-1281.
2. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations
3. The numerical computation of turbulent flows
4. ON THE CALCULATION OF TURBULENT HEAT TRANSPORT DOWNSTREAM FROM AN ABRUPT PIPE EXPANSION
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