Computational study of wing deformation and sting interference effects with the CAE-AVM test case

Author:

KURSAKOV Innokentiy,KAZHAN EgorORCID,GEBBINK Roy

Funder

Ministry of Education and Science of the Russian Federation

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference22 articles.

1. The development of a framework for CFD validation and best practice: the QNET-CFD knowledge base;Hirsch;Chin J Aeronaut,2006

2. CFD V & V and open benchmark database;Bai;Chin J Aeronaut,2006

3. Viscous transonic airfoil workshop compendium of results;Holst;J Aircraft,1998

4. Schmitt V, Charpin F. Pressure distributions on the ONERA-M6-Wing at transonic Mach numbers, experimental data base for computer program assessment. Paris: AGARD; 1979. Report No.: AGARD AR 138.

5. Laflin KR, Vassberg JC, Wahls RA, Morrison JH, Brodersen O, Radowitz M, et al. Summary of data from the Second AIAA CFD Drag Prediction Workshop. Reston: AIAA; 2004. Report No.: AIAA-2004-0555.

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