A problem in scheduling theory
โ Scribed by S.I. Vasilenko
- Publisher
- Elsevier Science
- Year
- 1983
- Weight
- 351 KB
- Volume
- 23
- Category
- Article
- ISSN
- 0041-5553
No coin nor oath required. For personal study only.
โฆ Synopsis
- MacCORMACK R.W., The effect of viscosity in hypervelocity impact cratering. AIAA Paper, No.69-354, 1969. 4. KOSYKH A.P. and MINAILOS A.N., Investigation of through-calculation methods for problems of supersonic aerodynamics. Uch. zap. TsAGI, No.l, 9-17, 1976. 5. VINOGRADOV V.A., IVANOV M.A. and KRAIKO A.N., On the application of difference "throughcalculation" schemes for computing flow with shock waves.
In: Numerical methods of the mechanics of a continuous medium (Chislennye metody mekhaniki sploshnoi sredy), Vol.8, No.2, 5-11, Nauka, Novosibirsk, 1977. 6. ALALYKIN G.B. et al. Solution of one-dimensional problem of gas dynamics on mobile meshes (Reshenie odnomernykh zadach gazovoi dinamiki v podvizhnykh setkakh). Nauka, Moscow,1970. 7. MORETTI G., Three-dimensional supersonic steady flows with any number of imbedded shocks.
AIAA Paper No.74-i0, 1974. 8. BERLYAND A.T.and FROST V.A.~ A method for calculating two-dimensional supersonic flows with automatic separation of discontinuities and a stepwise approximation of the rarefaction waves.
In: Numerical methods of the mechanics of a continuous medium (Chislennye metody mekhaniki sploshnoi sredy), Vol.3, No.3, 3-12, Nauka, Novosibirsk, 1972. 9. BERLYAND A.T., Computer realization of the numerical method of calculating two-dimensional supersonic flows with automatic separation of discontinuities.
Tr. TsAGI, No.1807, 3-28, Moscow, 1977. I0. KOTOV V.D., ALGOL-60 program for calculating the two-dimensional supersonic flow of a non-viscous gas in a channel by the method of constructing a plane graph.
Tr. TsAGI, No. 1807, 29-86, Moscow, 1977. ii. SHCHENNIKOV S.A., Calculation of the transients in an air-intake channel during throttling. In: Trans. of Joint Scientific Readings on Space Travel. Theory and construction of aircraft engines (Tr. ob'edinennykh nauchnykh chtenii po kosmonavtike. Teoriya i konstruktsiya dvigatelei letatel'nykh apparatov) In-t istorii estestvoznaniya i tekh. AN SSSR, 233-240, 1981. 12. BABENKO K.I.+, et al.
Ideal three-dimensional flow of a gas past smooth bodies (Prostranstvennoe obtekanie gladkikh tel ideal'nym gazom) Nauka, Moscow, 1964. 13. KUTLER P. and LOMAX H., A systematic development of the supersonic flow fields over and behind wings and wing-body configurations using a finite-difference approach. AIAA Paper No.71-99, 1971. Russian translation in: Numerical methods in mechanics of fluids. (Chisl. metody v mekh. zhidkostei, Mir, Moscow, pp.126-134, 1973). 14. ABBETT M.J., Boundary condition computational procedures for inviscid supersonic steady flow field calculations. Final Rept. Aerotherm. Corp. Mt. View, California, No.71-41, 1971. 15. LOBANOVSKII Yu.I., On the monotonization of finite-difference solutions for through-calculation methods, zh. vychisl. Mat. mat. Fiz., 19, 4, 1063-1069, 1979.
Translated by WC.
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