Aviation Dictionary
پسایی که به صورت طبیعی در اثر شکل سطح مقطع یک ایرفویل ایجاد میشود، نیروی بازدارنده ای که از بهم خوردن جریان یکنواخت هوا توسط مقطع جسم ناشی میشود ، پسای فرم برای صفحهای که به موازات جریان است حداقل و برای صفحه عمود بر جریان حداکثر میباشد .
Form Drag or Pressure Drag or Profile Drag arises because of the shape of the object. The general size and shape of the body are the most important factors in form drag; bodies with a larger presented cross-section will have a higher drag than thinner bodies; sleek ("streamlined") objects have lower form drag. Form drag follows the drag equation, meaning that it increases with velocity, and thus becomes more important for high-speed aircraft.
Form drag depends on the longitudinal section of the body. A prudent choice of body profile is essential for a low drag coefficient. Streamlines should be continuous, and separation of the boundary layer with its attendant vortices should be avoided.