Computation of choked and supersonic turbomachinery flows by a modified potential method
Author:
Affiliation:
1. Concordia University, Montreal, Quebec, Canada
2. Computer Dynamics Inc., Virginia Beach, Virginia
3. Pratt& Whitney Canada Inc., Longueuil, Quebec, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8897
Reference9 articles.
1. Artificial Compressibility Methods for Numerical Solutions of Transonic Full Potential Equation
2. Finite Element Solutions of Transonic Flow Problems
3. Progress in finite element techniques for transonic flows
4. Section G. The Supersonic Compressor
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. REDUCED-ORDER MODELS OF UNSTEADY TRANSONIC VISCOUS FLOWS IN TURBOMACHINERY;Journal of Fluids and Structures;2000-11
2. Transonic viscous-inviscid interaction by a finite element method;International Journal for Numerical Methods in Fluids;1991-07-20
3. A new formulation for unsteady compressible Euler equations;9th Computational Fluid Dynamics Conference;1989-06-13
4. Unsteady Aerodynamics for Turbomachinery Aeroelastic Applications;Unsteady Transonic Aerodynamics;1989-01-01
5. Reply by Authors to T. C. Adamson Jr., J. Mace, and A. F. Messiter;AIAA Journal;1986-09
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