Turbulence-induced disturbances and their evolution to stall onset in a compressor cascade using large eddy simulation

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Open-loop control of combustion instabilities in a full-scale annular ramjet combustor using linear genetic programming

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Experimental study of overall roughness surface effect on hypersonic boundary layer transition of yawed cone

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Impact of multiscale flow structures on mixing and losses in turbine blade tip region

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Validation of time–space collocation method for simulating asymmetric unsteady flows in eccentric compressors

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A novel small perturbation analytical model to investigate temperature control characteristics of spacecraft thermal systems in frequency domain

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Mixing and initiating mechanism of internal injection oblique detonation engine

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Numerical investigation of flow features and aero-optical effects of turrets with different bottom cylinder heights in a transonic flow

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Integrated rapid analysis method for thermal environment in aircraft cabin

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Broadband performance of multi-degree-of-freedom septum liners under high-velocity grazing flows

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Flow combustion characteristics and performance of Al powder-fueled water ramjet engine under different injection schemes

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An analytical study for detonation wave boundary layer interactions under reflections

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Impact of spring pressure on ignition and combustion of electrically controlled solid propellant

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Damage behavior of aircraft radome under high-speed jet impact

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Predicting and minimizing twin-propeller noise: Hessian matrix and Fourier-Frobenius matrix analysis in improved propeller signatures theory

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Aeroelastic characteristics and vibration reduction method of NTBT rotor with TEF technology

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Fluid-structure coupling characteristics of membrane under supersonic conditions

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Neural network control for mitigating actuator delay in ATR engines using predictive compensation and stability reward

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A satellite layout-structure integrated optimization method based on thermal metamaterials

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Fully coupled fluid–structure interaction of diaphragm rupture in high-pressure-ratio shock tunnels

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