EROS — a common European Euler code for the analysis of the helicopter rotor flowfield

Author:

Renzoni Piergiovanni,D'Alascio Alessandro,Kroll Norbert,Peshkin Dave,Hounjet Michael H.L.,Boniface Jean-Christophe,Vigevano Luigi,Allen Christian B.,Badcock Ken,Mottura Lorenzo,Schöll Eberhard,Kokkalis Anastasios

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference66 articles.

1. Solution of the unsteady Euler equations for fixed and rotor wing configurations;Sankar;AIAA J. Aircraft,1986

2. Agarwal RK, Deese JE. Euler calculations for flowfield of a helicopter rotor in hover. Proceedings of the AIAA 4th Applied Aerodynamics Conference, AIAA-86-1782, June 1986.

3. Kroll N. Computation of the flow fields of propellers and hovering rotors using the Euler equations. Proceedings of the 12th European Rotorcraft Forum, Garmish-Partenkirchen, Germany, September 1986.

4. Krämer E, Hertel J, Wagner S. Computation of subsonic and transonic helicopter rotor flow using Euler equations. Proceedings of the 13th European Rotorcraft Forum, Arles, France, 1987.

5. Landgrebe AJ. New direction in rotorcraft computational aerodynamics research in the U.S. Proceedings of the AGARD FDP Aerodynamics and Aeroacoustics of Rotorcraft Symposium, AGARD-CP-552, Berlin, Germany, August 1994.

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