揚力 (Lift)
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Definition
気流に垂直に作用し、航空機を空中に保持する空気力学的な力。
揚力とは?
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.
仕組み
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.
航空における重要性
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.
実際の影響
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
V速度
決定速度、回転速度、最低安全上昇速度などの重要な飛行段階の境界を定義する標準化された基準対気速度。
ライトフライヤー
オーヴィル・ライトとウィルバー・ライトの兄弟が設計・製作した世界初の動力飛行機。1903年12月17日にノースカロライナ州キティホークで4回の短い飛行に成功した。
地面効果
翼と地面の間の気流圧縮により、地面近くを飛行する航空機が経験する揚力の増加と抗力の減少。
失速
翼が臨界迎え角を超え、突然かつ急激な揚力の喪失が起こる状態。
後方乱気流
飛行中の航空機の後方に残される回転渦で、後続機に深刻な危険をもたらす。
抗力
飛行方向と平行かつ反対方向に作用し、航空機の運動に抵抗する空気力学的な力。
迎え角(AoA)
翼の翼弦線と流入気流との角度で、発生する揚力の量を決定する。