Some improvements of hybrid trim method for a helicopter rotor in forward flight
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[1] B. Kulfan. Universal Parametric Geometry Representation Method , 2008 .
[2] 정기훈,et al. Numerical Predictions of Rotorcraft Unsteady Air-Loadings and BVI Noise By using a Time-Marching Free-Wake and Acoustic Analogy , 2005 .
[3] Domenico Quagliarella,et al. An aerothermodynamic design optimization framework for hypersonic vehicles , 2019, Aerospace Science and Technology.
[4] P. Roe. Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes , 1997 .
[5] W. K. Anderson,et al. Comparison of Finite Volume Flux Vector Splittings for the Euler Equations , 1985 .
[6] Renliang Chen,et al. Trim investigation for coaxial rigid rotor helicopters using an improved aerodynamic interference model , 2019, Aerospace Science and Technology.
[7] Lakshmi N. Sankar,et al. Recent Improvements to a Hybrid Method for Rotors in Forward Flight , 2000 .
[8] A. Jameson,et al. Lower-upper Symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations , 1988 .
[9] Chen Friedman,et al. Robust trim procedure for rotorcraft configurations , 2015 .
[10] Yongjie Shi,et al. A study of coaxial rotor aerodynamic interaction mechanism in hover with high-efficient trim model , 2019, Aerospace Science and Technology.
[11] Mark Potsdam,et al. High-Fidelity Structural Loads Analysis of the ONERA 7A Rotor , 2017 .
[12] Zhou Ye,et al. A High-efficiency Trim Method for CFD Numerical Calculation of Helicopter Rotors , 2017 .
[13] Hyeonsoo Yeo,et al. Design and aeromechanics investigation of compound helicopters , 2019, Aerospace Science and Technology.
[14] Damiano Casalino,et al. Rotorcraft blade-vortex interaction noise prediction using the Lattice-Boltzmann method , 2019, Aerospace Science and Technology.
[16] Donald F. Specht,et al. A general regression neural network , 1991, IEEE Trans. Neural Networks.