양력 (Lift) (Lift)
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Definition
기류에 수직으로 작용하여 항공기를 공중에 유지시키는 공기역학적 힘.
What Is Lift?
Lift is the aerodynamic force that acts perpendicular to the relative airflow and supports an aircraft in flight. It is the fundamental force that opposes gravity and allows heavier-than-air machines to become airborne. Without sufficient lift, no aircraft — from a Cessna 172 to an Airbus A380 — can remain aloft.
How It Works
Lift is generated primarily by the wings as air flows over and under them. Two complementary principles explain its generation:
- Bernoulli's Principle: The wing's cambered (curved) upper surface forces air to travel a longer path than the flatter lower surface. This accelerates the upper airflow, reducing pressure above the wing. The higher pressure beneath the wing pushes upward, producing lift.
- Newton's Third Law: The wing deflects incoming air downward. The reaction force pushes the wing — and the aircraft — upward.
Lift (L) is calculated as: L = ½ × ρ × V² × S × CL, where ρ is air density, V is airspeed, S is wing area, and CL is the coefficient of lift. This formula shows that doubling airspeed quadruples lift — a critical relationship for pilots during takeoff and approach.
Significance in Aviation
Lift determines an aircraft's maximum takeoff weight, cruise altitude, and approach speed. Wing design — including aspect ratio, camber, and sweep — is optimized to maximize lift while minimizing drag. High-lift devices such as flaps and slats increase the wing's CL during low-speed flight, allowing aircraft to operate at manageable V-speeds on shorter runways.
The angle of attack directly controls lift up to the critical AoA, beyond which a stall occurs. Pilots must manage this relationship constantly, especially during takeoff rotation and final approach.
Real-World Impact
The Boeing 747-400 generates approximately 900,000 lbf of lift at maximum takeoff weight — enough to keep 412 tonnes airborne across the Pacific. The Airbus A380's 845 m² wing area is specifically designed to generate adequate lift at relatively low approach speeds, reducing stress on airframe and runway. In contrast, the Concorde used a delta wing that generated lift through vortex flow rather than classical Bernoulli effects, allowing it to cruise efficiently at Mach 2.
Related Terms
받음각 (AoA)
날개의 시위선과 유입 기류 사이의 각도로, 발생하는 양력의 양을 결정한다.
항력 (Drag)
비행 방향과 반대로 평행하게 작용하여 항공기의 운동에 저항하는 공기역학적 힘.
지면 효과 (Ground Effect)
날개와 지면 사이의 기류 압축으로 인해 지면 근처에서 비행하는 항공기가 경험하는 양력 증가 및 항력 감소 현상.
실속 (Stall)
날개가 임계 받음각을 초과하여 갑작스럽고 급격한 양력 손실이 발생하는 상태.
V-속도 (V-Speeds)
결정 속도, 이륙 회전 속도, 최소 안전 상승 속도 등 중요한 비행 단계 경계를 정의하는 표준화된 기준 대기속도.
후류 난류 (Wake Turbulence)
비행 중인 항공기 뒤에 남겨지는 회전 와류로, 뒤따르는 항공기에 심각한 위험을 초래한다.
라이트 플라이어 (Wright Flyer)
오빌·윌버 라이트 형제가 설계·제작한 최초의 동력 비행 항공기로, 1903년 12월 17일 노스캐롤라이나주 키티호크에서 네 차례의 짧은 비행을 성공시켰다.