Calculation of unsteady transonic flows using the integral equation method
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1978-13
Reference12 articles.
1. Airfoils and Planar Wings,'' AFFDL-TR-75-10, 1975. 55 'Weatherhill, W. H., Ehlers, F. E., and
2. Implicit finite-difference computations of unsteady transonic flows about airfoils, including the treatment of irregular shock-wave motions
3. 5Yu. N. J. Seebass. A. R. and Ballhaus. W. F. "An Implicit Shock Fitting Scheme far Unsteady Transonic Flow Computations,"AIM Paper No. 77-633, 1977.
Cited by 4 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. Unsteady transonic aerodynamics and aeroelasticity;A Modern Course in Aeroelasticity;1995
2. Calculation of unsteady small disturbance transonic flow at arbitrary reduced frequency using an extended integral equation method;24th Structures, Structural Dynamics and Materials Conference;1983-05-02
3. Calculation of unsteady transonic flows with shocks by field panel methods;AIAA Journal;1982-06
4. Transonic Panel Method to Determine Loads on Oscillating Airfoils with Shocks;AIAA Journal;1981-05
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