| Performance analysis of a centimeter scale Tesla turbine for micro air vehicles SS Arindam Mandal International conference of Electronics, Communication and Aerospace …, 2017 | 11 | 2017 |
| Aerodynamic performance of a tandem wing configuration inspired from dragonfly gliding flight for MAV application R Adak, A Mandal, S Saha Conference on Fluid Mechanics and Fluid Power, 409-418, 2022 | 1 | 2022 |
| Stepped aerospike for enhanced drag reduction using multiple intermediate shocks ADK A. Mandal, S. Majumder, S. Saha Shock Waves 32, 485–495, 2022 | 1 | 2022 |
| Reynolds-averaged Navier–Stokes assisted direct numerical simulation of low Reynolds number flow over airfoils R Adak, A Mandal, S Saha Physics of Fluids 36 (12), 2024 | | 2024 |
| Direct numerical simulations of Dragonfly-inspired Tandem Wing Configuration at Low Reynolds Number R Adak, A Mandal, S Saha Bulletin of the American Physical Society, 2024 | | 2024 |
| Numerical optimization and compatibility assessment of millimeter-scale Tesla turbines in ultra-micro gas turbines A Mandal, R Adak, S Saha Bulletin of the American Physical Society, 2024 | | 2024 |
| Experimental and numerical investigation of the effect of inlet and outlet configurations on the performance enhancement of a 100 Watts-class Tesla turbine A Mandal, R Adak, S Saha Sādhanā 49 (1), 83, 2024 | | 2024 |
| Effect of aerospike geometry variation on drag reduction A Mandal, S Saha Скоростной транспорт будущего: перспективы, проблемы, решения, 194-195, 2022 | | 2022 |
Sandeep SahaAssociate Professor, Indian Institute of Technology Kharagpur在 alumni.imperial.ac.uk 的电子邮件经过验证
