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#Haixin Chen
Aeroacoustic Prediction of a Multi-Element Airfoil Using Wall-Modeled Large-Eddy Simulation
飞机研究与设计实验室(AEROlab) , 清华大学
Multi-Objective Aerodynamic-Structural Optimization of Supercritical Wing of Wide Body Aircraft
飞机研究与设计实验室(AEROlab) , 清华大学
Transonic Nacelle Aerodynamic Optimization Based on Hybrid Genetic Algorithm
飞机研究与设计实验室(AEROlab) , 清华大学
A Hybrid Aerodynamic Optimization Algorithm Based on Differential Evolution and RBF Response Surface
飞机研究与设计实验室(AEROlab) , 清华大学
U or V Shape: Dissipation Effects on Cylinder Flow Implicit Large-Eddy Simulation
飞机研究与设计实验室(AEROlab) , 清华大学
An Aircraft Conceptual Design and Optimization Platform and Its Application for Nature Laminar Flow Aircraft Study
飞机研究与设计实验室(AEROlab) , 清华大学
Numerical Research on Aerodynamic Efficiency of a VTOL GFS UAV
飞机研究与设计实验室(AEROlab) , 清华大学
Drag prediction method of powered-on civil aircraft based on thrust drag bookkeeping
飞机研究与设计实验室(AEROlab) , 清华大学
Improvement of Infrared Horizon Detector Using Two-dimensional Infrared Temperature Distribution Model
飞机研究与设计实验室(AEROlab) , 清华大学
Multi-objective aerodynamic optimization of supercritical wing with substantial pressure constraints
飞机研究与设计实验室(AEROlab) , 清华大学
Grid Convergence Study on a Finite Volume Code NSAWET
飞机研究与设计实验室(AEROlab) , 清华大学
Grid-Convergence Study of Two-Dimensional Euler Solutions
飞机研究与设计实验室(AEROlab) , 清华大学
NSAWET Results of the Dual Separate Flow Reference Nozzle from AIAA PAW02
飞机研究与设计实验室(AEROlab) , 清华大学
Performance Prediction of Conical Nozzle using Navier-Stokes Computation
飞机研究与设计实验室(AEROlab) , 清华大学
Performance Prediction of Conical Nozzle Using Navier–Stokes Computation
飞机研究与设计实验室(AEROlab) , 清华大学
A Thrust Drag Bookkeeping Method based on Computational Fluid Dynamics
飞机研究与设计实验室(AEROlab) , 清华大学
A Computational Fluid Dynamics Study of Circumferential Groove Casing Treatment in a Transonic Axial Compressor
飞机研究与设计实验室(AEROlab) , 清华大学
Numerical investigation of the casing treatment mechanism with a single circumferential groove
飞机研究与设计实验室(AEROlab) , 清华大学