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Ashish Vashishtha
Ashish Vashishtha
Lecturer, South East Technological University, Carlow Campus, IRELAND
Verified email at setu.ie - Homepage
Title
Cited by
Cited by
Year
Experimental study of overexpanded co-flowing jets
H Sharma, A Vashishtha, E Rathakrishnan, P Lovaraju
The Aeronautical Journal 112 (1135), 537-546, 2008
262008
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
202009
Twin-vortex flow physics
H Sharma, A Vashishtha, E Rathakrishnan
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2008
112008
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
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
82021
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
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
52021
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
42012
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
32022
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
32021
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
doi: https://doi. org/10.15866/irease. v13i1 18282, 25-39, 2020
3*2020
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
32008
Novel Mechanism of Instability Control using a Tapered Spike in Hypersonic Flow
A Vashishtha, S Khurana
AIAA AVIATION 2021 FORUM, 2543, 2021
22021
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
22018
Base Pressure Control by using Ribs in Subsonic and Sonic Suddenly Expanded Flows
S Yedlapalli, A Vashishtha, K Vijayaraja, E Rathakrishnan
22008
Investigation of a modified circular nozzle for cold spray applications
AK Sharma, A Vashishtha, D Callaghan, SR Bakshi, M Kamaraj, ...
ITSC 2023, 235-241, 2023
12023
Mach number dependence of flow instability around a spiked body
A Vashishtha, S Khurana
AIP Conference Proceedings 2584 (1), 2023
12023
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