01.2 - Aircraft Design and Integrated System (Applications)
NUMERICAL INVESTIGATION ON THE AERO-PROPULSION EFFECT OF DISTRIBUTED PROPULSION FOR V/VTOL APPLICATION
S. Song¹, S. Deng¹, Q. Li, AVIC General Aircraft Research Institute, China; H. Qiao¹, Y. Lu¹; ¹Nanjing University of Aeronautics and Astronautics, China
The aim of this paper is to first explore the benefits and its inner method for various EDF integrated concepts. Then for a given-flight envelope V/STOL high speed aircraft, a best concept will be chosen. Finally, large amounts of calculation could provide enough reference data for the evaluation in general design phase.rn