Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Ivan E. Cherepanov"'
Autor:
Darya Hrolikova, Vladimir Modorskiy, Anton O. Mikryukov, Danila S. Maksimov, S. L. Kalyulin, Ivan E. Cherepanov, A. V. Babushkina
Publikováno v:
Perm National Research Polytechnic University Aerospace Engineering Bulletin. :83-91
Autor:
Vladimir Ya. Modorskii, Grigory F. Masich, Ivan E. Cherepanov, S. L. Kalyulin, Anton O. Mikryukov, Mikhail I. Sokolovskii, Danila S. Maksimov
Publikováno v:
Communications in Computer and Information Science ISBN: 9783030553258
The paper presents a promising direction of developing and using the cyberinfrastructure focused on pipelined/parallel data processing on a supercomputer of the experimental setup being developed at Perm National Research Polytechnic University, a sm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f69f3df0834e705a5486f23e73e2b005
https://doi.org/10.1007/978-3-030-55326-5_24
https://doi.org/10.1007/978-3-030-55326-5_24
Autor:
S. L. Kalyulin, Danila S. Maksimov, Anton O. Mikryukov, Ivan E. Cherepanov, A. V. Babushkina, Vladimir Ya. Modorskii
Publikováno v:
Communications in Computer and Information Science ISBN: 9783030553258
The problem of vibrations arising during the operation of gas transmittal unit compressors is an urgent task in designing a rotor constructor. Existing approaches do not allow predicting the vibration probability in every operating mode. The article
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa51cfd8f5b33fefc171b95afa8d3d36
https://doi.org/10.1007/978-3-030-55326-5_23
https://doi.org/10.1007/978-3-030-55326-5_23
Autor:
Vasily Yu. Petrov, S. L. Kalyulin, Vladimir Ya. Modorskii, Danila S. Maksimov, Anton O. Mikryukov, Ivan E. Cherepanov
Publikováno v:
Communications in Computer and Information Science ISBN: 9783030553258
Creation of multi-mode aero-cooled climatic wind tunnels (ACCWT) for testing the icing of aircraft structures is an urgent task of modern aircraft construction. The ACCWT nozzle is one of its most complex elements in terms of design. The article pres
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7697824dbbddbf6b7793c254d6c91d27
https://doi.org/10.1007/978-3-030-55326-5_22
https://doi.org/10.1007/978-3-030-55326-5_22
Publikováno v:
AIP Conference Proceedings.
Numerical modeling of the icing process on the wing profile NACA 0012 is conducted. The influence of speed, pressure and temperature of the incoming gas-dynamic flow, the attack angle of the profile, the water content of the medium, the wing surface