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Which of the following would not increase net thrust?

  • A.Better expansion at the nozzle exit
  • B.An increase in flight speed at constant exhaust velocity
  • C.An increase in exhaust velocity
  • D.An increase in mass flow

Answer: B

Correct answer: An increase in flight speed at constant exhaust velocity

Net thrust depends on the increment \( \dot{m}(V_e - V_0) \), so raising the flight speed while the exhaust velocity stays put narrows that increment and reduces the thrust. This is the thrust lapse with speed. The other three all increase it: more mass flow, a higher exhaust velocity, or better expansion at the nozzle exit recovering the pressure term.

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