Experimental study of overexpanded co-flowing jets H Sharma, A Vashishtha, E Rathakrishnan, P Lovaraju The Aeronautical Journal 112 (1135), 537-546, 2008 | 27 | 2008 |
Breathing blunt-nose concept for drag reduction in supersonic flow A Vashishtha, E Rathakrishnan Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2009 | 19 | 2009 |
Twin-vortex flow physics H Sharma, A Vashishtha, E Rathakrishnan Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2008 | 12 | 2008 |
Study of Direct Gas Injection into stagnation zone of Blunt Nose at Hypersonic Flow P Harmon, A Vashishtha, D Callaghan, C Nolan, R Deiterding AIAA Propulsion and Energy 2021 Forum, 3529, 2021 | 10 | 2021 |
Study of shock shape in front of concave, convex and Flat Arc in Hypersonic Flow A Vashishtha, Y Watanabe, K Suzuki JAXA special publication: JAXA-SP-14-010, 127-132, 2015 | 9 | 2015 |
Study of bow-shock instabilities in front of hemispherical shell at hypersonic Mach number 7 A Vashishtha, Y Watanabe, K Suzuki 45th AIAA Fluid Dynamics Conference, 2638, 2015 | 9 | 2015 |
Drag Control by Hydrogen Injection in Shocked Stagnation Zone of Blunt Nose A Vashishtha, D Callaghan, C Nolan IOP Conference Series: Materials Science and Engineering 1024, 012110, 2021 | 7 | 2021 |
Bow-shock instability and its control in front of hemispherical concave shell at hypersonic Mach number 7 A Vashishtha, Y Watanabe, K Suzuki TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES …, 2016 | 7 | 2016 |
Pulsating Flow Investigation for Spiked Blunt-Nose Body in Hypersonic Flow and its Control A Vashishtha, S Khurana AIAA Scitech 2021 Forum, 0839, 2021 | 6 | 2021 |
Oblique Detonation Wave Control with O3 and H2O2 Sensitization in Hypersonic Flow A Vashishtha, S Panigrahy, D Campi, D Callaghan, C Nolan, R Deiterding Energies 15 (11), 4140, 2022 | 5 | 2022 |
Study of intake ports design for ultra low cost (ULC) gasoline engine using STAR-CD A Vashishtha, B Rathinam, L Delahaye, F Ravet, F Justet SAE Technical Paper, 2012 | 5 | 2012 |
Numerical investigation of detonation propagation through small orifice holes A Vashishtha, D Callaghan, C Nolan, R Deiterding Transactions on Aerospace Research 2021 (3), 17-33, 2021 | 4 | 2021 |
Characteristics of sonic and supersonic co-flow jets H Sharma, A Vashishtha, P Lovaraju, E Rathakrishnan 2nd International Conference on Recent Advances in Experimental Fluid Mechanics, 2008 | 4 | 2008 |
Investigation of a modified circular nozzle for cold spray applications AK Sharma, A Vashishtha, D Callaghan, SR Bakshi, M Kamaraj, ... International Thermal Spray Conference 84536, 235-241, 2023 | 3 | 2023 |
Particle Acceleration Through Coaxial Co-Flow Nozzles for Cold Spray Applications A Kumar Sharma, A Vashishtha, D Callaghan, C Nolan, S Bakshi, ... Thermal Spray 2022: Proceedings from the International Thermal Spray …, 2022 | 3* | 2022 |
On unsteady flow analysis of a round spike blunt nose afterbody in Mach 6 flow A Vashishtha, S Khurana IOP Conference Series: Materials Science and Engineering 1024 (1), 012017, 2021 | 3 | 2021 |
Flow-Field and Performance Study of Coaxial Supersonic Nozzles Operating in Hypersonic Environment M Samara, A Vashishtha, Y Watanabe, K Suzuki doi: https://doi. org/10.15866/irease. v13i1 18282, 25-39, 2020 | 3* | 2020 |
Novel Mechanism of Instability Control using a Tapered Spike in Hypersonic Flow A Vashishtha, S Khurana AIAA AVIATION 2021 FORUM, 2543, 2021 | 2 | 2021 |
Numerical Study of Detonation Driven Miniature Shock Tubes using OpenFoam A Vashishtha, S Rao MV 5th National Symposium on Shock Waves, TBRL, Chandigarh, INDIA Feb 26-28, 2018, 2018 | 2 | 2018 |
Base Pressure Control by using Ribs in Subsonic and Sonic Suddenly Expanded Flows S Yedlapalli, A Vashishtha, K Vijayaraja, E Rathakrishnan | 2 | 2008 |