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Prof Srisha Rao M V

vidwan id: 66343
Male

Associate Professor, Aerospace Engineering
Indian Institute of Science Bangalore

Expertise

  • Aerospace Engineering

Publications

Total Articles 41
Books 0
Proceedings 0

Publications

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Scopus

Citations 643
h-index 16

CrossRef

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Citations 523
h-index 14
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Bio

Exciting research is being carried out in both external and internal gasdynamic phenomena at high Mach numbers. Dominantly experimental tools are employed to study the phenomena including high speed visualization and optical flow diagnostics such as PIV and PLIF. Several aspects of the unsteady non-linear nature of shock-shear layer interactions are being explored. Some of the interesting problems are supersonic mixing and its enhancement, complex nozzles, shock-mixing layer interactions, flow c

Personal Details

  • Male
  • Associate Professor , Indian Institute of Science Bangalore
  • Bangalore, Karnataka, India
PhD
Other Institute 2014
ME
Other Institute 2008
BE
Other Institute 2006
Associate Professor Jul 2022 – Present
Indian Institute of Science Bangalore | Aerospace Engineering
Assistant Professor Apr 2018 – Jul 2022
Indian Institute of Science Bangalore | Aerospace Engineering

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Co-Authors (7)

Gopalan

Prof Gopalan Jagadeesh

Indian Institute of Science Bangalore

K. P. J.

Prof K. P. J. Reddy

Indian Institute of Science Bangalore

Pramod

Dr Pramod Kumar

Indian Institute of Science Bangalore

S.

Dr S. Saravanan

Indian Institute of Science Bangalore

S.

Prof S. Asokan

Indian Institute of Science Bangalore

S K

Dr S K Karthick

Indian Institute of Technology Hyderabad

B G

Dr B G Sudarshan

R V College of Engineering, Bangalore

Scholarly Work

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Yogeshwaran, G

University Indian Institute of Science Bengaluru
Year 2018
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Scholarly Publications

Response of a Flat Plate to Fluid-Structure Interaction in Hypersonic Flow

Open Access
Conference Paper
Authors: Ahuja K.;Srisha Rao M.V.

Response of a cantilevered plate to shock impingement in hypersonic flows

Open Access
Conference Paper
Authors: Ahuja K.;Srisha Rao M.V.

Effect of Isolator length in Nozzle – Isolator Interaction in Co-flow set up recurrent in Hypersonic Propulsion systems

Open Access
Conference Paper
Authors: Himakar A.B.;Rengasamy K.;Rao S.M.V.

Low-frequency unsteadiness of recompression shock structures in the diffuser of supersonic ejectors

Open Access
Article

Performance evaluation of air ejectors using artificial neural network approach

Open Access
Article

Optimization of Conceptual Design of Air Breathing Hypersonic Vehicle

Open Access
Conference Paper
Authors: Deepak K.;Wangikar A.U.;Chathura G.R.;Khadtare S.S.;Rao A.G.;Yogesh Y.;Mukesh M.;Rao S.M.V.

Artificial neural network model for single-phase real gas ejectors

Open Access
Article

Artificial neural network based shape optimization of supersonic ejectors in the critical flow regime

Open Access
Article