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Ashish Vashishtha
Ashish Vashishtha
Lecturer, South East Technological University, Carlow Campus, IRELAND
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Experimental study of overexpanded co-flowing jets
H Sharma, A Vashishtha, E Rathakrishnan, P Lovaraju
The Aeronautical Journal 112 (1135), 537-546, 2008
272008
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
192009
Twin-vortex flow physics
H Sharma, A Vashishtha, E Rathakrishnan
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2008
122008
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
102021
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
92015
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
92015
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
72022
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
72021
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
72016
Pulsating Flow Investigation for Spiked Blunt-Nose Body in Hypersonic Flow and its Control
A Vashishtha, S Khurana
AIAA Scitech 2021 Forum, 0839, 2021
62021
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
52012
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
4*2022
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
42021
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
42008
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
32023
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
32021
Flow-Field and Performance Study of Coaxial Supersonic Nozzles Operating in Hypersonic Environment
M Samara, A Vashishtha, Y Watanabe, K Suzuki
International Review of Aerospace Engineering (IREASE) 18282, 25-39, 2020
3*2020
Numerical investigation of the impact of injectors location on fuel mixing in the HIFiRE 2 Scramjet combustor
SK Palateerdham, LN Phaneendra Peri, A Ingenito, A Vashishtha
Aerospace Europe Conference 2023, 2023
22023
Numerical study of oblique detonation wave control for fuel blends
R Kore, A Vashishtha
57th 3AF International Conference Aero 2023, 2023
22023
Novel Mechanism of Instability Control using a Tapered Spike in Hypersonic Flow
A Vashishtha, S Khurana
AIAA AVIATION 2021 FORUM, 2543, 2021
22021
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