Which outcome occurs when combustion instability escalates inside a pulse detonation engine's cycle?

💡 Explanation

Uncontrolled pressure rise and deflagration is the result because detonation transitions occur due to the Zeldovich-von Neumann-Döring (ZND) model, therefore leading to destructive overpressure, rather than enhanced cooling, damping, because other cycles manage steady thrust.

• Which effect results when closely spaced microstructures cause spectral shifts?
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