Nozzle and cavity wall cooling limitations on specific impulse of a gas-core nuclear rocket
Nozzle and cavity wall cooling limitations on specific impusle of gas-core nuclear rocket engine
Kascak, A. F.↗
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Nozzle and cavity wall cooling limitations on specific impusle of gas-core nuclear rocket engine
A new approach to structural failure detection and localization is introduced based on acoustic reflections. It is shown that the cross-sectional areas of structural elements can be computed directly in terms of the reflection coefficients of an optimal finite impulse response Wiener filter realized in lattice form.