Understanding Shock Wave Interaction With Obstacles

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Key Takeaways about Shock Wave Interaction With Obstacles

  • Wind tunnel Mach numer 2.0 Boundary layer over the flat surface is thin. Ramp angle is changed from 20 to 30 degrees.
  • This is an unsteady viscous computation of a
  • This video demonstrates the propagation
  • Dynamic Behaviour of Materials Course URL: https://swayam.gov.in/nd1_noc19_me65/preview Prof. Prasenjit Khanikar Dept. of ...
  • Effect of transient

Detailed Analysis of Shock Wave Interaction With Obstacles

Shock wave interaction An unsteady Fluid-Structure

CFD Computation of a

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