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EXPERIMENTAL STUDY ON NO TAIL ROTOR (NOTAR) HELICOPTER
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作者 王华明 张呈林 罗晓平 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2001年第1期53-58,共6页
The circulation contr ol tail boom is a new technology used as an anti-torque system for the no tail rotor helicopter. In order to study the effect of the different parameters on th e circulation control tail boom, t... The circulation contr ol tail boom is a new technology used as an anti-torque system for the no tail rotor helicopter. In order to study the effect of the different parameters on th e circulation control tail boom, two models with the different circulation contr ol tail booms are designed and constructed. The experiments are introduced in th is paper by measuring the pressure distribution on the models in wind tunnel and under main rotor, respectively. By analyzing and discussing the experimental re sults, the effects of the momentum coefficient, the slot′s geometry parameters and the freestream velocity on the aerodynamic forces of the circulation control tail boom have been expounded, and the reasonable explanations about the test r esult have been given in theory. 展开更多
关键词 HELICOPTER no tail rot or (NOTAR) circulation control
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