Abstracts

Below you can find the abstracts, please click the abstract number to view the pdf file.

A zip-file containing all abstracts can be downloaded here

Monday 1 July

10:30 - 10:50 [4] Wave diffractions over a cavity, S Vishnu Prasad, Rajesh G, Anbu Serene Raj C and Vinoth P, Dept. of Aerospace Engineering, IIT Madras, Chennai, India

10:50 - 11:10 [12] On the Shock Wave Propagation Dynamics Following Sudden Area Expansion, Yoav Gichon, Jibu Tom Jose, Hemanth Chandravamsi, Yigal Evron and Omri Ram, Faculty of Mechanical Engineering, Technion-Israel Institute of Technology, Haifa 3200003, Israel

11:30 - 11:50 [25] Shock Wave Propagation with Shear-layer and Surface Interaction during Transonic Deceleration, Irshaad Mahomed, Hamed Roohani, Irvy M.A. Gledhill and Beric W. Skews, School of Mechanical, Industrial, and Aeronautical Engineering, Faculty of Engineering, University of Witwatersrand, South Africa

11:50 - 12:10 [10] Shock Wave Interaction Characteristics produced by Liquid Jet Injection in a Supersonic Crossflow, Srinivas M V V and Arun Kumar R, Dept. of Mechanical Engineering, Indian Institute of Technology Jodhpur, Jodhpur-342030, India

12:10 - 12:30 [14] Effect of Upstream Injection on a Confined Supersonic Cavity Flow, Sumit Lonkar, Shiv Prateek S, Nimesh Thakor and Pratikash Panda, Dept. of Aerospace Eng., Indian Institute of Science, India

14:00 - 14:20 [13] Shock interaction in a Transverse injection from a Bumped Surface in a Supersonic Crossflow, Spandan Maikap and Arun Kumar R, Dept. of Mechanical Engineering, Indian Institute of Technology Jodhpur, Jodhpur-342030, India

14:20 - 14:40 [8] Shock Boundary Layer Interaction in Internal Flow: Dependence on the Method of Throttling, Balaji A Himakar and Srisha M V Rao, Dept. of Aerospace Engineering, Indian Institute of Science, Bangalore, India

14:40 - 15:00 [27] Particle Image Velocimetry of a Highly Separated Transitional Shock-Wave/Boundary-Layer Interaction Philipp L. Nel, Anne-Marie Schreyer, Ferry F. J. Schrijer and Bas W. van Oudheusden RWTH Aachen University, Aachen, Germany

15:00 - 15:20 [17] An experimental study to investigate the effect of dynamic variation of the shock strength on shock boundary layer interaction, Rahul R. Kapse and T. M. Muruganandam, Department of Aerospace Engineering, Indian Institute of Technology Madras, Tamil Nadu, India

15:50 - 16:10 [3] Shock refractions at an air-water interface in weak and strong incident shock regimes, Anbu Serene Raj C, Rajesh G, A Sameen and Ben-Dor Gabriel, Dept. of Aerospace Engineering, IIT Madras, Chennai, India

16:10 - 16:30 [18] Experimental investigations on the interaction between impinging shock and cavity shear layer, Madavan Dwarakesh, Abhishek Kumar, Samiayyan Pandian and Rengarajan Sriram, Dept. of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, India

16:30 - 16:50 [20] Study on the Interaction of Cavity Flow with Oscillating Shock Train, Dandu Sri Sruthi, Madavan Dwarakesh, Sundararajan L. N. Desikan and Rengarajan Sriram, Indian Institute of Technology Madras, Chennai-600036, India

16:50 - 17:10 [31] Shock wave boundary layer interaction control with shock control bumps, Jane Bulut, Ferry Schrijer and Bas van Oudheusen, Aerospace Engineering Faculty, Delft University of Technology, The Netherlands

Tuesday 2 July

10:10 - 10:30 [7] Numerical Investigation of Suction Effects on Interaction and Transition of Laminar/Transitional SWBLI in a Hypersonic Double Wedge, DiviaHarshaVardini R C, Rajesh G, and Ikhyun Kim, Dept. of Aerospace Engineering, IIT Madras, India

10:30 - 10:50 [9] Spanwise properties of a hypersonic shock wave/boundary layer interaction on a heated surface, Divek Surujhlal, Alexander Wagner, Tobias Ecker and Jan Martinez Schramm, Spacecraft Department, Institute for Aerodynamics and Flow Technology, German Aerospace Center (DLR)" Germany

10:50 - 11:10 [21] Experiments on Control of Large Amplitude Shock Train Oscillations using Bleed, Anuj Nigam, Abhishek Kumar, Sundararajan. L. N. Desikan and Rengarajan Sriram Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, India

11:30 - 11:50 [6] Unsteady shock reflections over an oscillating ramp using the Meshless method, Shubham K Vyas, Divya Harshavardhini, Vinoth P., and Rajesh G., Dept. of Aerospace Engineering, IIT Madras, India

11:50 - 12:10 [19] Extinguishing detonation in pipelines transporting gaseous fuels, Zbigniew A. Walenta and Agnieszka M. Słowicka, Institute of Fundamental Technological Research, Polish Academy of Sciences, Warszawa, Poland

12:10 - 12:30 [16] Review of Ongoing Chemical Kinetics Studies at Laboratory for Hypersonic and Shock Wave Research, IISc, Chaitanya Bhoir, Deepak Singh, Arunan Elangannan and Jagadeesh Gopalan, Dept. of Aerospace Engineering, Indian Institute of Science, India

14:00 - 14:20 [30] Shock Control Bumps for Mitigation of Transonic Buffet Loads on an Airfoil, Alessandro D'Aguanno, Alessandro Corduas, Ferry Schrijer and Bas van Oudheusen Aerospace Engineering Faculty, Delft University of Technology, The Netherlands

14:20 - 14:40 [2] Mach Stem Height Estimation in Strong Reflection Domain for Overexpanded Jets, Vinoth P, Reva Dhillon, Thara Reshma I V and Rajesh G, Dept. of Aerospace Engineering, IIT-Madras, Chennai, India

14:40 - 15:00 [23] Passive flow control in confined supersonic cavities of varying impinging shock strengths, Sreejita Bhaduri, Ashoke De and Mohammed I. Sugarno, Dept. of Aerospace Engineering, Indian Institute of Technology Kanpur, India

15:00 - 15:30 [11] On the convergence of cylindrical shock wave, Sourabh Bhardwaj, Nicholas Apazidis and Michael Liverts Dept. of Engineering Mechanics, KTH Royal Institute of Technology, Sweden

15:50 - 16:10 [1] Reconstruction of flow field from sparse data using physics informed neural network Sivaprasad Gangadharan and Rajesh Gopalapillai, Dept. of Aerospace Engineering, Indian Institute of technology, Chennai, Tamil Nadu, India

16:10 - 16:30 [22] Assessment of Local Artificial Diffusivity and Gradient-Based Reconstruction Methods for High-Speed Flows, Ritu Raj Kumar, Shivam Saini, Nagabhushana Rao Vadlamani, and Amareshwara Sainadh Chamarthi Indian Institute of Technology, Madras, Chennai-600036, India

16:30 - 16:50 [28] Effects of ridge-type spanwise heterogeneous roughness on shock- wave/turbulent boundary layer interactions, Wencan Wu, Luis Laguarda, Davide Modesti, and Stefan Hickel Aerospace Engineering Faculty, Delft University of Technology, The Netherlands

16:50 - 17:10 [26] Analysis for analog system of detonation with two step chemical reaction model, Yuanxiang Sun, Beijing Institute of Technology, Beijing, China

Wednesday 3 July

10:10 - 10:30 [29] Intermittent shock oscillations and Kelvin Helmholtz vortices past a supersonic micro ramp Sumit Sunil Tambe, Ferry Schrijer and Bas van Oudheusden, Dept. of Aerospace Engineering, Indian Institute of Science, India

10:30 - 10:50 [24] Research on Ultrafast Response Pressure- Sensitive Paint Suitable for Measuring Unsteady Shock Wave Phenomena in Atmospheric Pressure Environments, Daiju Numata, Yuma Kawamata, Takeru Kawashima and Kiyonobu Ohtani, Dept. of Aeronautics and Astronautics, School of Engineering, Tokai University, Japan

10:50 - 11:10 [15] Experimental study on the effect of leading edge bluntness on an osculating waverider in hypersonic flow, P V Karthikeya Bharadwaj, Agnivo Ghosh, Gopalan Jagdeesh, S Sarvanan, K Nagashetty, Srisha MV Rao "Department of Aerospace Engineering, Indian Institute of Science, Bengaluru, 560012, India

11:30 - 11:50 [5] Prediction of Pseudosteady shock refraction over air-water interface using Fourier Neural Operator, Sivaprasad G, Kushi Borwal, Anbu Serene Raj C and Rajesh G, Dept. of Aerospace Engineering, Indian Institute of technology, Chennai, Tamil Nadu, India