Improvements to an Euler aerodynamic method for transonic flow analysis
Author:
Affiliation:
1. Lockheed Aeronautical Systems Company, Burbank, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45717
Reference22 articles.
1. JMehta, U. and Lomax, H. "Reynolds Averaged Navier-Stokes Computations of Transonic Flows-The State of the Art,"Progress in Astronautics and Aeronautics: Transonic Aerodynamics, Vol.81, edited by D. Nixon,AIAA, New York, 1982, pp.297-375.
2. A multi-grid method for transonic wing analysis and design
3. Numerical solution of transonic wing flowfields
4. Progress in Finite-Volume Calculations for Wing-Fuselage Combinations
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