Conservative full-potential model for unsteady transonic rotor flows
- 1 February 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (2), 193-198
- https://doi.org/10.2514/3.9608
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Solution of transonic flow past rotor blades using the conservative full potential equationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Unsteady transonic full potential solutions for airfoils encountering vortices and gustsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Numerical solution of the full-potential equation for rotors and oblique wings using a new wake modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Interactions of airfoils with gusts and concentrated vortices in unsteady transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- A conservative finite difference algorithm for the unsteady transonic potential equation in generalized coordinatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Computation of subsonic and transonic flow about lifting rotor bladesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979