An Euler solver for calculating the flowfield of a helicopter rotor in hover and forward flight
By: R. K. Agarwal and J. E. Deese.
Contributors: Deese, J. E.; AIAA
Publisher: American Institute of Aeronautics and Astronautics
Published: 1987
Place of publication: New York
Subjects: Euler equations of motion; Helicopters; Rotary wings
Notes: Bibliographical references: p. 8-9.

Source: AIAA 19th Fluid Dynamics, Plasma Dynamics and Lasers Conference, June 8-10, 1987, Honolulu, Hawaii