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- W2146296032 abstract "VACUUM THRUST OF JET PROPULSION DEVICE The ideal vacuum thrust function is used to determine the local thrust of aerospace engine. Method of thrust determination from measured pressures are applied to the model M=2.5 supersonic combustor. In this application, measured pressures from the experiments in the University of Michigan are used to determine the local The ideal thrust equation for a jet propulsion device can be derived from the general form of Newton's second law(i.e., force equals the time rate of change of momentum)." @default.
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- W2146296032 date "2002-07-07" @default.
- W2146296032 modified "2023-10-16" @default.
- W2146296032 title "Assessment of Thrust from Pressure Measurements of Supersonic Combustor" @default.
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- W2146296032 doi "https://doi.org/10.2514/6.2002-4016" @default.
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