Further development of the IAR two-variable boundary-interference correction method for low-speed wind tunnel data
Author:
Affiliation:
1. Inst. for Aerospace Research, Ottawa, Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-884
Reference17 articles.
Cited by 6 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. Advances in Wall Interference Corrections for Two-Dimensional Lifting Bodies;AIAA Journal;2023-12
2. Application of the Two-Variable Correction Method to Measurements in an Open-Jet Test Section;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08
3. Assessment of Boundary Interference in Open Test Section Wind Tunnels Using Successive Over-Relaxation;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10
4. Streamwise Momentum Analysis of Subsonic Wall Interference on Flat-Plate Wings at High Angles of Attack;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05
5. Recent developments in the calculation of low-speed solid-walled wind tunnel wall interference in tests on large models;Progress in Aerospace Sciences;2003-08
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