Implicit finite-difference computations of unsteady transonic flows about airfoils, including the treatment of irregular shock-wave motions
Author:
Affiliation:
1. NASA, Ames Research Center; U.S. Army, Air MobilityResearch and Development Laboratory, Moffett Field, Calif.
2. Informatics Corp., Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-205
Cited by 20 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. Aeroelasticity Research at Wright-Patterson Air Force Base (Wright Field) from 1953-1993;Journal of Aircraft;2003-09
2. Effective method of calculating the wave drag of solids of revolution in the transonic range;Journal of Applied Mechanics and Technical Physics;1995-05
3. Action of wind gusts and weak shocks on an airfoil in a transonic stream;Journal of Applied Mechanics and Technical Physics;1993
4. The spectrum and the stability of the Chebyshev collocation operator for transonic flow;Mathematics of Computation;1988
5. Full-potential solutions for transonic flows about airfoils with oscillating flaps;22nd Aerospace Sciences Meeting;1984-01-09
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