Time-iterative solutions of viscous supersonic nozzle flows
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10030
Reference20 articles.
1. Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
2. An upwind algorithm for the parabolized Navier-Stokes equations
3. Assessment of a parabolic analysis for axisymmetric internal flows in rocket and turbomachinery ducts
4. An accurate, stable, explicit, parabolized Navier-Stokes solver for high speed flows
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