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CAESES > 2021 > May

Propulsion System Intake Duct for High Mach Number Regimes
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Propulsion System Intake Duct for High Mach Number Regimes

FRIENDSHIP SYSTEMS
12. May 2021
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The present case study investigates a hypothetical intake duct geometry for a TBCC propulsion system, which channels high-speed air from the freestream into the engine and converts the dynamic energy into high pressure by making use of a series of compression shocks.

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