Computation of Three Dimentional Flows about aircraft configurations

Computers & Fluids - Tập 1 - Trang 185-195 - 1973
F. Marconi1, M. Salas1
1Grumman Aerospace Corporation Bethpage, New York, U.S.A.

Tài liệu tham khảo

Moretti, 1969, The choice of a time-dependent technique in gas dynamics, PIBAL Report No. 69-26 Moretti, 1969, Importance of boundary conditions in numerical treatment of hyperbolic equations, Phys. Fluids, 12, 10.1063/1.1692426 G. Moretti, Thoughts and after about shock computations, to be published as a PIBAL report. Moretti, 1972, A complete numerical technique for the calculation of three-dimentional inv iscid supersonic flows, AIAA Paper No. 72-192 Courant, 1928, Ueber die partiellen Differenzgleichungen der mathematishen Physik, Math, Ann., 100, 32, 10.1007/BF01448839 MacCormack, 1969, The effects of viscosity in hypervelocity impact cratering, AIAA Paper No. 69-354 Moretti, 1966, A time dependent computational method for blunt body flows, AIAA, J4 Moretti, 1966, Three-dimentional flow around blunt bodies, AIAA, J5 Moretti, 1967, Inviscid flow field about pointed cone at angle of the attack, AIAA, J5 Prokop, 1972, Investigation of the effects of airframe design on inlet flow fields, AFFDL-TR-72-11, 1 Walkdeu, 1972, Application of a pseudo-viscous method to the calculation of the steady supersonic flow past a wasted body, Int. J. Numeric Meth. Engng., 5 Kutler, 1972, Computations of space shuttle flow fields using non-centered finite-difference schemes, AIAA Paper No. 72-193 Kutler, 1972, Numerical computation of multi-shocked three-dimentional supersonic flow fields with real gas effects, AIAA Paper No. 72-702