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- W2322205654 abstract "Thrust calculation is extremely straightforward for steady propulsion systems, thus the tendency to simply apply the same procedure to unsteady propulsion devices exists. The eect of ignoring the unsteady term in the axial momentum equation when assessing the specific thrust and/or specific impulse of an unsteady propulsion system is examined. Unsteady terms are analytically calculated based on locally steady phenomena and validated against a time-accurate numerical solution for single detonation tube open at only one end. Calculating and storing the unsteady terms increases computational demands, therefore it is important to understand when unsteady terms significantly contribute to specific thrust and impulse. Based on a fundamental understanding of unsteady thrust terms the decisions to calculate or ignore terms for a particular application can be justified." @default.
- W2322205654 created "2016-06-24" @default.
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- W2322205654 date "2004-06-26" @default.
- W2322205654 modified "2023-09-23" @default.
- W2322205654 title "Deconstructing Detonation: Analytical Calculation of Unsteady Thrust in a PDE" @default.
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- W2322205654 doi "https://doi.org/10.2514/6.2004-3395" @default.
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