Simulation of 3D Flows of Propulsion Systems Using an Efficient Low Diffusion E-CUSP Upwind Scheme-Reference-Cited by-同舟云学术

Simulation of 3D Flows of Propulsion Systems Using an Efficient Low Diffusion E-CUSP Upwind Scheme

Published:2004-06-26 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Hu Zongjun¹,Zha Gecheng¹

Affiliation:

1. University of Miami

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4082

Reference16 articles.

1. Approximate Riemann solvers, parameter vectors, and difference schemes

2. 2Jameson, A. "Analysis and Design of Numerical Schemes for Gas Dynamics I: Artificial Diffusion, Upwind Biasing, Limiters and Their Effect onAccuracyandMultigrid ConvergenceinTransonic andHypersonic Flow," AIAA Paper93-3359,71993.

3. ANALYSIS AND DESIGN OF NUMERICAL SCHEMES FOR GAS DYNAMICS, 1: ARTIFICIAL DIFFUSION, UPWIND BIASING, LIMITERS AND THEIR EFFECT ON ACCURACY AND MULTIGRID CONVERGENCE

4. ANALYSIS AND DESIGN OF NUMERICAL SCHEMES FOR GAS DYNAMICS, 2: ARTIFICIAL DIFFUSION AND DISCRETE SHOCK STRUCTURE

5. 5Hänel, D., Schwane, R., and Seider, G. "On the Accuracy of Upwind Schemes for the Solution of the Navier-Stokes Equations," AIAA Paper 87-1105CP,1987.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Simulation of the Aerodynamics of Waveriders Based on Shock Waves of Various Shapes;Fluid Dynamics;2023-08

2. Conceptual Design and Study of "Engineless" Airplane Using Co-Flow Jet Airfoil;25th AIAA Applied Aerodynamics Conference;2007-06-15

3. A Low Diffusion E-CUSP Upwind Scheme for Transonic Flows;34th AIAA Fluid Dynamics Conference and Exhibit;2004-06-19