rockets propellant, thermodynamic processes and state, processes of gas dynamics in propellant, multicomponents of substances mixture, programming languages
Subject:
rockets propellant, mathematics, physics. information technology
Main publications:
R. R. Nazyrova, N. B. Ponomarev, “IT-tekhnologii modelirovaniya realnosti rabochikh tel v protsessakh zhidkostnykh raketnykh dvigatelei”, Inzhenernyi zhurnal: nauka i innovatsii, 2013, № 4, 69–85
V. E. Alemasov, A. F. Dregalin, R. R. Nazyrova, “Termodinamika vysokotemperaturynkh protsessov: fizicheskie, matematicheskie i programmnye osnovy otsenki”, Izvestiya AN. Energetika, 1998, № 3, 7–24
R. R. Nazyrova, Issledovanie operatsii v otsenke termodinamicheskikh kharakteristik, ABAK, Kazan, 1999, 198 ñ.
R. R. Nazyrova, “Ob otsenke parametrov termodinamicheskikh sistem na osnove gilbertovykh i banakhovykh prostranstv”, Kraevye zadachi aerogidromekhaniki i ikh prilozheniya, Trudy Matematicheskogo tsentra imeni N. I. Lobachevskogo, 7, Izd-vo KGU, Kazan, 2000, 237–245
R. R. Nazyrova, “K voprosu o spetsialnykh mnozhestvakh i funktsiyakh”, Geometricheskaya teoriya funktsii i kraevye zadachi, Trudy Matematicheskogo tsentra im. N. I. Lobachevskogo, 13, Kazan, 2000, 117–120
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