A STUDY OF WINGLET AND AERODYNAMIC INTERFERENCES IN 3 D VISCOUS FLOW AROUND A FLYING BOAT IN GROUND EFFECT
عنوان مقاله: A STUDY OF WINGLET AND AERODYNAMIC INTERFERENCES IN 3 D VISCOUS FLOW AROUND A FLYING BOAT IN GROUND EFFECT
شناسه ملی مقاله: ISME15_055
منتشر شده در پانزدهمین کنفرانس سالانه مهندسی مکانیک در سال 1386
شناسه ملی مقاله: ISME15_055
منتشر شده در پانزدهمین کنفرانس سالانه مهندسی مکانیک در سال 1386
مشخصات نویسندگان مقاله:
Hossein Afshar - Former Graduate Student Dept. of Mech. Eng. Shiraz University
Mohammad Mahdi Alishahi - Prof. of Mech. Eng Dept. of Mech. Eng, Shiraz University
خلاصه مقاله:
Hossein Afshar - Former Graduate Student Dept. of Mech. Eng. Shiraz University
Mohammad Mahdi Alishahi - Prof. of Mech. Eng Dept. of Mech. Eng, Shiraz University
Studying different configurations and deciding about aerodynamic interferences has always been a time consuming and expensive task in the course of aerodynamic design of flight vehicles. Disadvantages multiply when using experimental tools for complicated objects flying close to ground. Large scale CFD simulation is another choice of modest time and expense. In this study, the flow field about a complete flying-boat in ground effect is resolved. The influences of using winglet in ground and out of ground effects are compared and it is shown that ground affects this influence to a large extent. It is also shown that with careful shaping of the body and using a step underneaththe body a propulsive force can be produced in vicinity of the ground. However, this causes an increase in drag force in free flight.
کلمات کلیدی: WIG، CFD، Ground Effect، Aerodynamics، Parallel Processing
صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/28706/