000 01905nab a2200337 c 4500
001 vtls000620482
003 RU-ToGU
005 20210922093505.0
007 cr |
008 180131|2017 xxu s a eng d
024 7 _a10.1063/1.5009883
_2doi
035 _ato000620482
040 _aRU-ToGU
_brus
_cRU-ToGU
245 1 0 _aGas flow calculation method of a ramjet engine
_cK. Kostyushin, A. Kagenov, I. Eremin [et.al.]
504 _aБиблиогр.: 12 назв.
520 3 _aAt the present study calculation methodology of gas dynamics equations in ramjet engine is presented. The algorithm is based on Godunov`s scheme. For realization of calculation algorithm, the system of data storage is offered, the system does not depend on mesh topology, and it allows using the computational meshes with arbitrary number of cell faces. The algorithm of building a block-structured grid is given. Calculation algorithm in the software package “FlashFlow” is implemented. Software package is verified on the calculations of simple configurations of air intakes and scramjet models.
653 _aпрямоточные реактивные двигатели
653 _aуравнения газовой динамики
653 _aГодунова схема
655 4 _aстатьи в журналах
_9745982
700 1 _aKostyushin, Kirill V
_9142520
700 1 _aEremin, Ivan V
_9121414
700 1 _aZhiltsov, Konstantin N
_9479528
700 1 _aShuvarikov, Vladimir
_9142521
700 1 _aKagenov, Anuar M
_9142519
773 0 _aAIP Conference Proceedings
_d2017
_gVol. 1799. P. 060012-1-060012-8
_x0094-243X
852 4 _aRU-ToGU
856 7 _uhttp://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000620482
908 _aстатья
999 _c430769