Dr Vamsi Krishna Talluri
Post-Doctoral Fellow
| Aerospace Engineering
Technion, Israel
Haifa District
Expertise:
Aerospace Engineering
19
Publications
0
Projects
51
Scopus Citations
47
CrossRef
4 Years 10 Months Total Experience
Scopus
51
Citations
4
h-index
CrossRef
47
Citations
4
h-index
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Professional Recognition
International Travel Fellowship
2022
Council of Scientific and Industrial Research (CSIR, Govt.India)
International Travel Fellowship
2023
Science and Engineering Research Board (SERB),DST
Funded trip to International seminar for Young scientists
2023
TsAGITech Center, Zhukovsky, Russia. from Government of Russia.
Second Prize in project completion in workshop for Young scientist and Specialists during Green Flight: Future Green Aviation Technologies
2023
TsAGITech Center, Zhukovsky, Russia.
Trust for Advancement of Aerodynamics in India (TAAI) Student Registration Support
2023
Trust for Advancement of Aerodynamics in India (TAAI)
Editor’s Pick, Phys. Fluids (Vol. 36, Issue 11, 116105
2024
Physics of Fluids Journal
Community & Membership
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Personal Details
Doctor of Philosophy
2024
Indian Institute of Technology, Roorkee
Master of Engineering
2016
Central Institute of Mining and Fuel Research
Bachelor of Technology
2014
P P Savani School of Management
Post-Doctoral Fellow
Apr 2024 – Present
Technion, Israel
| Aerospace Engineering
Junior Research Fellow
Aug 2016 – Dec 2018
Birla Institute of Technology, Ranchi
| Department of Space Engineering and Rocketry
Engineering and Technology
Scholarly Work
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Scholarly Publications
Heat Transfer Measurements in an Axisymmetric Open Cavity at Hypersonic Speeds
Effect of Plate Distance on Steady and Unsteady Characteristics of Impinging Rectangular Jet
On the fluidic behavior of an over-expanded planar plug nozzle under lateral confinement
On the unsteady dynamics of partially shrouded compressible jets
On the Dynamics of Imploding and Exploding Spherical Shock Wave Inside a Shock Tube
Shock Wave Boundary Layer Interactions Over a Forward-Facing Step at Mach 6
Experimental study of impinging plug nozzle jet using a vortex generator
Experimental and Numerical Investigation of LeadingEdge Bluntness on Shock Boundary layer Interaction Inside a Scramjet Inlet at Mach 6
Showing 1 to 8 of 19 publications