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Fluiddynamik
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Self-Similar-Structure–Based All-Speed Genuinely Two-Dimensional Riemann Solver
Combustion Intensification Mechanism in a Vortex-Tube Reactive Flow
Introducing a Multi-Modal Plasma Actuator for Turbulent Flow Actuation
Aeroacoustic Source Potential Based on Poisson’s Equation
Computational Study of Airfoil Design Parameters and Sensitivity Analysis for Dynamic Stall
Point-Collocation Nonintrusive Polynomial Chaos Method for Stochastic Computational Fluid Dynamics
Numerical Study of Supersonic Jet Characteristics of Underwater Solid Rocket Engine
Hypersonic International Flight Research Experimentation Flight 2 Unstart Reliability Analysis
Accurate and Robust Hybrid HLLC Riemann Solver on Triangular Grids
Acoustic Modeling Using the Aeroacoustic Wave Equation Based on Pierce’s Operator
Influence of Single Roughness Element on Hypersonic Boundary-Layer Transition of Cone
Performance Improvement of Winged Compound Helicopter Due to Differential Flap Deflections
Sensitivity-Based Geometric Parametrization and Automatic Scaling for Aerodynamic Shape Optimization
Analysis of Plume Infrared Signatures of S-Shaped Nozzle Configurations of Aerial Vehicle
Design-Variable Hypernetworks for Flowfield Emulation and Shape Optimization of Compressor Airfoils
Numerical Study on Wind-Driven Thin Water Film Runback on an Airfoil