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Unformatted text preview: "Assuming the mass flow and inlet and exit velocities remain constant". Without this phrase, most of you (correctly) assumed that as the exit pressure was reduced, the exit velocity would increase, increasing thrust. It was my intention in asking the problem however, to have you focus only on the term in the thrust equation related to the pressure forces around the engine. Class performance (2001):...
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This note was uploaded on 01/28/2012 for the course AERO 16.01 taught by Professor Markdrela during the Fall '05 term at MIT.
- Fall '05