Engineering, 05.11.2020 18:50, genyjoannerubiera

Actual performance characteristics of the Lockheed SR-71 °Blackbird" reconnaissance aircraft were classified. However, it was thought to cruise atM=3.3 at 26 km altitude. Calculate the aircraft flight speed for these conditions. Determine the local isentropic stagnation pressure. Evaluate the stagnation pressure sensed by a probe on the aircraft. What is the maximum air temperature at stagnation points on the aircraft structure?

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Actual performance characteristics of the Lockheed SR-71 °Blackbird" reconnaissance aircraft were cl...