Progress in Finite-Volume Calculations for Wing-Fuselage Combinations
- 1 November 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (11), 1281-1288
- https://doi.org/10.2514/3.50883
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Numerical Calculation of Transonic Potential Flow about Wing-Body CombinationsAIAA Journal, 1979
- A systematic procedure for generating useful conformal mappingsInternational Journal for Numerical Methods in Engineering, 1978
- Accelerated Iterative Calculation of Transonic Nacelle FlowfieldsAIAA Journal, 1977
- A finite volume method for transonic potential flow calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Numerical calculation of the transonic flow past a swept wing. [FLO 22]Published by Office of Scientific and Technical Information (OSTI) ,1977
- Cartesian Mesh Solution for Axisymmetric Transonic Potential Flow Around InletsAIAA Journal, 1977
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974
- Estimation of the Relaxation Factor for Small Mesh SizeMathematical Tables and Other Aids to Computation, 1956