AERODYNAMICS AND FLUID MECHANICS

Massachusetts Institute Of Technology

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MIT: AERODYNAMICS AND FLUID MECHANICS EXAM 2025 WITH ACCURATE SOLUTIONS
  • MIT: AERODYNAMICS AND FLUID MECHANICS EXAM 2025 WITH ACCURATE SOLUTIONS

  • Exam (elaborations) • 24 pages • 2025
  • 1. What is the relationship between throat static pressure and inlet static pressure in a converging duct? Throat static pressure is higher than inlet static pressure. Throat static pressure is lower than inlet static pressure. Throat static pressure fluctuates with inlet static pressure. Throat static pressure is equal to inlet static pressure. 2. In a nozzle designed for supersonic flow, if the throat mass flow rate is 10 kg/s, what could be the possible exit mass flow rate if the fl...
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