A Structured Mesh Euler and Interactive Boundary Layer Method for Wing/Body Configurations

Author:

Jie Li,Zhou Zhou

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference20 articles.

1. Accurate prediction of drag using Euler methods;Van Dam;Journal of Aircraft,1992

2. Civil aviation and the environment challenge;Green;The Aeronautical Journal,2003

3. Rear fuselage transonic flow characteristics for a complete wing-body configuration;Coustols;Journal of Aircraft,1997

4. Destarac D, Schmitt V. Recent progress in drag prediction and reduction for civil transport aircraft at ONERA. AIAA Paper 98-0137, 1998.

5. Destarac D. Far-field/near field drag balance and applications of drag extraction in CFD. VKI Lecture Series 2003, CFD-based Aircraft Drag Prediction and Reduction. National Institute of Aerospace, Hampton (VA); 2003.

Cited by 2 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. An interactive boundary layer modelling methodology for aerodynamic flows;International Journal of Numerical Methods for Heat & Fluid Flow;2013-10-28

2. Application of Parallel Computation in Numerical Simulation of Laser Propulsion;Applied Mechanics and Materials;2011-10

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