Overall Thrust of a RAMJET engine Calculator

The performance of a ramjet engine is typically characterized by key parameters that assess its efficiency and effectiveness in generating thrust. The performance of a ramjet engine can be evaluated using various metrics, including specific thrust, thermal efficiency, and overall thrust.

The overall thrust generated by a ramjet engine is the primary performance metric and depends on factors such as air mass flow rate and combustion efficiency.

Formula for thrust (T):

T=ṁ(VeV0)

Where:

  • T is the thrust generated by the engine (in Newtons, N).
  • ṁ is the air mass flow rate (in kilograms per second, kg/s).
  • Ve is the exhaust velocity of the engine (in meters per second, m/s).
  • V0 is the inlet velocity of the incoming air (in meters per second, m/s).

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