论文信息 - Numerical solutions of forward-flight rotor flow using an upwind method

Numerical solutions of forward-flight rotor flow using an upwind method

A finite-volume upwind algorithm for solving the three-dimensional Euler equations with a moving grid has been developed for computing helicopter forward-flight rotor flows. The computed pressure distributions and shock positions of high-speed rotor flow are compared with various experimental data as well as with other numerical results, and the agreement is encouraging

S. Obayashi | Chung-Lung Chen | W. Mccroskey

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