Euler calculations for flowfield of a helicopter rotor in hover
Author:
Affiliation:
1. McDonnell Douglas Research Laboratories, St. Louis, MO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1782
Reference4 articles.
1. Subsonic and Transonic Potential Flow over Helicopter Rotor Blades
2. Jijk = T1236 + T3867 +T1685 + T1348 + T3816, )
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1. Numerical Analysis of Maneuvering Rotorcraft Using Moving Overlapped Grid Method;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2008
2. A current density conservative scheme for incompressible MHD flows at a low magnetic Reynolds number. Part II: On an arbitrary collocated mesh;Journal of Computational Physics;2007-11
3. Computational analysis of effects of blade shapes on tip-vortices;Advances in Engineering Software;2003-05
4. EROS — a common European Euler code for the analysis of the helicopter rotor flowfield;Progress in Aerospace Sciences;2000-08
5. Development of a rotary wing multigrid Navier-Stokes CFD code based on TLNS3D code;12th Computational Fluid Dynamics Conference;1995-06-19
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