A higher order panel method for general analysis and design applications in subsonic flow
Part of the Lecture Notes in Physics book series (LNP, volume 59)
KeywordsSource Strength Subsonic Flow Vortex Sheet Wing Surface Singularity Strength
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.
Unable to display preview. Download preview PDF.
- 1.F. T. Johnson and P. E. Rubbert, “Advanced Panel-Type Influence Coefficient Methods Applied to Subsonic Flows”, AIAA Paper no. 75-50, January 20, 1975.Google Scholar
- 2.F. E. Ehlers, F. T. Johnson and P. E. Rubbert, “A Higher Order Panel Method for Linearized Supersonic Flows, AIAA Paper No. 76-381 (to be published July 15, 1976).Google Scholar
- 3.P. E. Rubbert and G. R. Saaris, “Review and Evaluation of a Three-Dimensional Lifting Potential Flow Analysis Method for Arbitrary Configurations”, AIAA Paper no. 72-188, January 1972.Google Scholar
© Springer-Verlag 1976