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Phillips, W. F., and Anderson, E. A., "Predicting the Contribution of Running Propellers to aircraft Stability Derivations," AIAA Paper 20020390, Jan. 2002. The z component of velocity induced by this model of the wingtip vortices, at the arbitrary point in space (x, y, z) is readily found from the biot-savart law to be wingspan wing tip vortex spacing wing lift co
- Author
- Gabriel Rodrigues Felix
- Language
- EN