Computing aerodynamic performance of a 2D iced airfoil - Blocking topology and grid generation-Reference-Cited by-同舟云学术

Computing aerodynamic performance of a 2D iced airfoil - Blocking topology and grid generation

Published:2002-01-14 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA Aerospace Sciences Meeting & Exhibit
language:
Short-container-title:

Author:

Chi X.¹,Slater J.²,Shih T.,Zhu B.,Addy H.,Choo Y.

Affiliation:

1. Michigan State Univ., East Lansing

2. NASA, Glenn Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-381

Reference14 articles.

1. Addy, H.E."Ice Accretions and Icing Effects for Modern Airfoils,"NASA/TP-2000-210031,April 2000.

2. Chung,JJ, Choo, Y.K., Reehorst,A.,Potapczuk, andSlater, J.

3. Choo,Y.K., Slater,J.W.,Henderson,T., Bidwell,C., Braun, D., and Chung J.J."User Manual for Beta Version of Turbo-GRD: A Software System for Interactive Two-Dimensional Boundary/Field Grid Generation,Modification, and Refinement,"NASA TM-1998-206631, 1998.

Cited by 11 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. Prediction of ice accretion and aerodynamic performance analysis of NACA 2412 aerofoil;The Aeronautical Journal;2023-04-28

2. Framework of Multiblock Structured Grid Smoothing Algorithms for Aircraft Configurations;Journal of Aircraft;2018-07

3. A framework for multi-block structured grid smoothing for 2D/3D aircraft configurations;23rd AIAA Computational Fluid Dynamics Conference;2017-06-02

4. Grid-Generation Algorithms for Complex Glaze-Ice Shapes Reynolds-Averaged Navier–Stokes Simulations;AIAA Journal;2016-03

5. Adaptive curvature control grid generation algorithms for complex glaze ice shapes RANS simulations;53rd AIAA Aerospace Sciences Meeting;2015-01-02