An implicit shock-fitting scheme for unsteady transonic flow computations
Author:
Affiliation:
1. Arizona, University, Tucson, Ariz.
2. Arizona, University, Tucson, Ariz.; U.S. Army, Air Mobility Research and Development Laboratory, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-633
Reference25 articles.
1. Ballhaus, W. F. and Lomax, H., 1975, "The Numerical Simulation of Low Frequency Unsteady Transonic Flow Fields", Lecture Notes in Physics, Springer-Verl ag, Vol. 35, pp. 57-63.
2. Unsteady Transonic Flows over an Airfoil
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1. Transonic kernel function method for unsteady flow calculations using a unified linear pressure panel procedure;21st Structures, Structural Dynamics, and Materials Conference;1980-05-12
2. Calculation of Unsteady Transonic Flows Using the Integral Equation Method;AIAA Journal;1978-09
3. Small Unsteady Perturbations in Transonic Flows;AIAA Journal;1978-08
4. A lifting surface theory based on an unsteady linearized transonic flow model;19th Structures, Structural Dynamics and Materials Conference;1978-04-03
5. Calculation of unsteady transonic flows using the integral equation method;16th Aerospace Sciences Meeting;1978-01-16
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