Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Krithika Vysaprasad"'
Autor:
V. R. Sanal Kumar, Vigneshwaran Sankar, Nichith Chandrasekaran, Vignesh Saravanan, Vishnu Natarajan, Sathyan Padmanabhan, Ajith Sukumaran, Sivabalan Mani, Tharikaa Rameshkumar, Hema Sai Nagaraju Doddi, Krithika Vysaprasad, Sharad Sharan, Pavithra Murugesh, S. Ganesh Shankar, Mohammed Niyasdeen Nejaamtheen, Roshan Vignesh Baskaran, Sulthan Ariff Rahman Mohamed Rafic, Ukeshkumar Harisrinivasan, Vivek Srinivasan
Publikováno v:
AIP Advances, Vol 14, Iss 10, Pp 109901-109901-2 (2024)
Externí odkaz:
https://doaj.org/article/e518810238654b81820a97f11439d1b3
Autor:
V. R. Sanal Kumar, Vigneshwaran Sankar, Nichith Chandrasekaran, Vignesh Saravanan, Vishnu Natarajan, Sathyan Padmanabhan, Ajith Sukumaran, Sivabalan Mani, Tharikaa Rameshkumar, Hema Sai Nagaraju Doddi, Krithika Vysaprasad, Sharad Sharan, Pavithra Murugesh, S. Ganesh Shankar, Mohammed Niyasdeen Nejaamtheen, Roshan Vignesh Baskaran, Sulthan Ariff Rahman Mohamed Rafic, Ukeshkumar Harisrinivasan, Vivek Srinivasan
Publikováno v:
AIP Advances, Vol 13, Iss 4, Pp 049901-049901-2 (2023)
Externí odkaz:
https://doaj.org/article/c6b9077d33044432976146762cd23f48
Autor:
V. R. Sanal Kumar, Vigneshwaran Sankar, Nichith Chandrasekaran, Vignesh Saravanan, Vishnu Natarajan, Sathyan Padmanabhan, Ajith Sukumaran, Sivabalan Mani, Tharikaa Rameshkumar, Hema Sai Nagaraju Doddi, Krithika Vysaprasad, Sharad Sharan, Pavithra Murugesh, S. Ganesh Shankar, Mohammed Niyasdeen Nejaamtheen, Roshan Vignesh Baskaran, Sulthan Ariff Rahman Mohamed Rafic, Ukeshkumar Harisrinivasan, Vivek Srinivasan
Publikováno v:
AIP Advances, Vol 8, Iss 2, Pp 025315-025315-22 (2018)
A closed-form analytical model is developed for estimating the 3D boundary-layer-displacement thickness of an internal flow system at the Sanal flow choking condition for adiabatic flows obeying the physics of compressible viscous fluids. At this uni
Externí odkaz:
https://doaj.org/article/47604f7b67e94eb2a99c9d3accb4cfe4
Autor:
Sasitharan Ambicapathy, A. Rakesh, N. D. Hemasai, VR Sanal Kumar, P. Sivaraj, Krithika Vysaprasad
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
In this paper diagnostic investigation of flow field characteristics of different cavity based scramjet combustors have been carried out for both non-reacting and reacting flows. The hydrogen fuel is injected at three different jet angles from ten di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1746f554b991e8bbcb9b15d05e1bb527
https://doi.org/10.2514/6.2014-3872
https://doi.org/10.2514/6.2014-3872