Ramjet Engine with Rotating Detonation Combustion System and Method for Operation
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United States of America
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Issued Date -
Feb 6, 2020
app pub date -
Aug 6, 2018
filing date -
Aug 6, 2018
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Abstract
A ramjet engine and system and method for operation is generally provided. The ramjet includes a longitudinal wall extended along a lengthwise direction. The longitudinal wall defines an inlet section, a combustion section, and an exhaust section. A fuel nozzle assembly is extended from the longitudinal wall. The fuel nozzle assembly defines a nozzle throat area. The fuel nozzle assembly is moveable along a radial direction to adjust the nozzle throat area based at least on a difference in pressure of a flow of fluid at an inlet of the inlet section and a pressure of the flow of fluid at the fuel nozzle assembly.
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