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Ice-proof bleed air preheating and turbine cooling bleed air precooling system for aircraft engine
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Spliced heat exchanger for high-speed air suction type engine
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Transonic compressor plane cascade with bionic sawtooth tail edge structure
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Transonic compressor plane cascade with bionic wavy structure leading edge
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A kind of fluidic oscillator array and its frequency synchronization method
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The damping structure Vibration Absorption Designing method of integral blade disk
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Double outer adaptive cycle engines of culvert
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Aero-engine overall performance slump evaluations and prediction technique based on data
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Thin-wall construction axial bending loading device
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The fan propeller of variable-diameter and established angle based on hydraulic-driven
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Using the engine blower and its diameter adjustment method of the variable-diameter of hydraulic-driven
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Across the medium flight device power device shared based on combustion chamber between grade and turbine water sky
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Across medium flight device power device based on empty water flow passage compact layout
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Aircraft engine oil cooling system and method
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Self contained internal combustion wave rotor igniter and method
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The conduit gas curtain extinguishing combustion chamber of radial fuel oil classification
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Main chamber triple channel dump diffuser
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Across the medium flight device power device sealed using medium sensing device and duct
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Obtain the method for numerical simulation in the flow field of potential flows
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The design method of high load capacity allowance camber is adjustable tandem cascade
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