Feng Qu

发表

A new all-speed flux scheme for the Euler equations

Feng Qu, Jiaojiao Chen, Di Sun, 2019, Comput. Math. Appl..

Investigation into the influences of the low-speed flows' accuracy on RANS simulations

Feng Qu, Di Sun, 2017 .

Numerical investigation of blunt body’s heating load reduction with combination of spike and opposing jet

J. Bai, Chao Yan, Feng Qu, 2018, International Journal of Heat and Mass Transfer.

An improvement on the AUSMPWM scheme for hypersonic heating predictions

Feng Qu, Di Sun, Guang Zuo, 2017 .

A study of parameter-free shock capturing upwind schemes on low speeds’ issues

J. Yu, Chao Yan, Feng Qu, 2014 .

A new Roe-type scheme for all speeds

Chao Yan, Feng Qu, Di Sun, 2015 .

Estimation and Analysis of Hybrid Laminar Flow Control on a Transonic Experiment

J. Bai, Feng Qu, Tianshi Cao, 2020 .

A study of multidimensional fifth-order WENO method for genuinely two-dimensional Riemann solver

J. Bai, Feng Qu, Di Sun, 2022, J. Comput. Phys..

A study of shock capturing methods for simulations of compressible turbulence\ with shock waves

Chao Yan, Feng Qu, Di Sun, 2017, 2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE).

WITHDRAWN: A robust and high-fidelity aerodynamic optimization design of truss-braced-wing aircraft with gradient-based method

Shiwei Ma, Junqiang Bai, Li Li, 2019, Aerospace Science and Technology.

A Review of Riemann Solvers for Hypersonic Flows

J. Bai, Feng Qu, Di Sun, 2021, Archives of Computational Methods in Engineering.

Investigation of all-speed schemes for turbulent simulations with low-speed features

Lingjiu Zhou, Chao Yan, Feng Qu, 2018 .

Poly-phase structural evolution of the northeastern Alxa Block, China: Constraining the Paleozoic-Recent history of the southern Central Asian Orogenic Belt

Feng Qu, Jin Zhang, Jinyi Li, 2020, Gondwana Research.

Numerical study of the hysteresis effect on the supercritical airfoil for the transonic circulation control

J. Bai, Feng Qu, Qing Wang, 2022, Aerospace Science and Technology.

Three-dimensional pore-scale study of the directional heat transfer in a high thermal conductivity carbon/carbon composite protection system

Hejun Li, Q. Fu, J. Bai, 2021 .

Schwinger pairs production in a soft-wall model

Feng Qu, Ding-fang Zeng, 2016, 1611.04009.

Multipoint Aerodynamic Shape Optimization of a Truss-Braced-Wing Aircraft

J. Bai, Feng Qu, Li Li, 2022, Journal of Aircraft.

Preliminary study on heat flux measurement data of TT-0 flight test

Feng Qu, Zheng Guo, Honggang Zeng, 2021 .

A hybrid multidimensional Riemann solver to couple self-similar method with MULTV method for complex flows

Feng QU, Di SUN, Junjie FU, 2021, Chinese Journal of Aeronautics.

A study of higher-order reconstruction methods for genuinely two-dimensional Riemann solver

Feng Qu, Junqiang Bai, Di Sun, 2021, J. Comput. Phys..

Improvement of the genuinely multidimensional ME-AUSMPW scheme for subsonic flows

Feng Qu, Di Sun, Qingsong Liu, 2021, Comput. Math. Appl..

A new genuinely two-dimensional Riemann solver for multidimensional Euler and Navier-Stokes Equations

Feng Qu, Junqiang Bai, Di Sun, 2019, Comput. Phys. Commun..

A genuinely two-dimensional Riemann solver for compressible flows in curvilinear coordinates

Feng Qu, Di Sun, Junqiang Bai, 2019, J. Comput. Phys..

A robust flux splitting method with low dissipation for all‐speed flows

Chao Yan, Feng Qu, Di Sun, 2017 .

A new flux splitting scheme for the Euler equations

Jian Yu, Feng Qu, Chao Yan, 2014 .

Numerical study of the suction flow control of the supersonic boundary layer transition in a framework of gas-kinetic scheme

J. Bai, Feng Qu, Di Sun, 2020 .

Numerical study of instabilities and compressibility effects on supersonic jet over a convex wall

J. Bai, Feng Qu, Di Sun, 2022, Journal of Fluid Mechanics.

An effective low dissipation method for compressible flows

Junqiang Bai, Di Sun, Chao Yan, 2020 .

Numerical investigation of the supersonic stabilizing parachute's heating loads

J. Bai, Chao Yan, Feng Qu, 2019, Aerospace Science and Technology.

A grid strategy for predicting the space plane's hypersonic aerodynamic heating loads

Feng Qu, Junqiang Bai, Di Sun, 2019, Aerospace Science and Technology.

An effective flux scheme for hypersonic heating prediction of re-entry vehicles

Feng Qu, Di Sun, Chao Yan, 2018, Computers & Fluids.

An efficient smoothness indicator mapped WENO scheme for hyperbolic conservation laws

Feng Qu, Xin Zhang, Chao Yan, 2022, Computers & Fluids.

An efficient adjoint method for the aero-stealth shape optimization design

Feng Qu, Xiaoyu Feng, Junqiang Bai, 2021 .

Effective high-order solver with thermally perfect gas model for hypersonic heating prediction

Chao Yan, Feng Qu, Li-Bin Ma, 2016 .

Shock-stable flux scheme for predicting aerodynamic heating load of hypersonic airliners

J. Bai, W. Kong, Feng Qu, 2019, Science China Physics, Mechanics & Astronomy.

Numerical study of interactions between shock waves and a circular or elliptic bubble in air medium

J. Bai, Feng Qu, Jiaojiao Chen, 2021 .

Numerical investigation of the unstart flow at off-design condition of REST inlet at a Mach of 4

J. Bai, Feng Qu, Di Sun, 2023, Aerospace Science and Technology.

A General NHPP Software Reliability Growth Model with Fault Removal Efficiency

Xiao-Zong Yang, Hong-Wei Liu, Feng Qu, 2005 .

An implicit large eddy simulation method based on all-speed schemes

J. Bai, Feng Qu, Di Sun, 2022, Comput. Math. Appl..

An effective all-speed Riemann solver with self-similar internal structure for Euler System

J. Bai, Feng Qu, Di Sun, 2022, Computers & Fluids.

A Review of Riemann Solvers for Hypersonic Flows

J. Bai, Feng Qu, Di Sun, 2021, Archives of computational methods in engineering : state of the art reviews.

A deep learning based prediction approach for the supercritical airfoil at transonic speeds

J. Bai, Feng Qu, Di Sun, 2021, Physics of Fluids.

Multi-objective aerodynamic optimization of two-dimensional hypersonic forebody-inlet based on the heuristic algorithm

J. Bai, Feng Qu, Di Sun, 2022, Aerospace Science and Technology.