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Maximum Pressure on Flat Plate at Mach 2.4 by Jefferson Manuel Medina Caceres is a document available to read on EtoBox.

What is Maximum Pressure on Flat Plate at Mach 2.4 about?

1. The document discusses three problems related to supersonic aerodynamics. The first problem asks to determine the maximum pressure and angle of attack for an attached shock wave on a flat plate in Mach 2.4 flow. The second compares the total pressure loss for slowing Mach 4 flow to subsonic through different shock systems. The third determines wave drag and lift coefficients for a supersonic aircraft model and computes the angle and sound pressure level of the sonic boom perceived on the ground.

Author

Jefferson Manuel Medina Caceres

Language

EN