Breakdown of the conservative potential equation
Author:
Affiliation:
1. NASA, Langley Research Center, Transonic Aerodynamics Div., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-367
Reference22 articles.
1. A comparative study of the nonuniqueness problem of the potential equation
2. Supercritical Wing Sections II
3. Plentovich, E. B., Ladson, C. L., and Hill, A. S. "Tests of a NACA 651-213 Airfoil in the NASA Langley 0.3-Meter Transonic Cryogenic Tunnel,11 NASA TM-85732, Feb. 1984.
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