今日介紹下Spinning~
Spinning 同spiral dive 雖然都係同轉圈有關,但係佢地唔一樣㗎~
首先要發生Spinning 就要有stall 出現左先,然後當其中一隻機翼比另一隻機翼stall 得更嚴重,aircraft nose 就會yaw 去more stalled 隻翼果邊。發生呢個情況嘅原因係飛機轉彎嘅時候超過左 critical AoA,同時間又用得太多/太少 rudder。

另外仲有一啲唔同嘅yawing force 會引致spinning,例如 multi engine 飛機發生engine failure,unbalanced fuel load (CG changes)
Spinning 嘅特徵分別有以下幾個:
1. 沿住 vertical spin axis 有 steep helical path 嘅 descent
2. 兩隻翼都超過 stall angle
3. 沿住 vertical spin axis 有high rate of rotation
4. Spinning可以係erect/inverted/flat 嘅狀態

Spin 嘅階段分別有3個:
1. Incipient spin (啱啱stall 完之後開始有rotation)
2. Fully developed spin (穩定嘅angular rotation rates, airspeed, vertical descent rate)
3. Spin recovery (anti spin forces 大過原本嘅spin force)
Recovery from a spin
1. Idle Power 目的係減少 engine torque 帶黎嘅 rotation force 同埋減少 altitude loss
2. Ailerons neutral 目的係將兩隻翼嘅AoA 變返一樣,從而減少rolling and yawing moment
3. 由 turn coordinator 可以睇到spin 嘅方向,然後apply 相反方向嘅rudder 就可以停左個spin & roll moment
4. 當個situation stabilized 之後就可以 full throttle,然後 gently 飛返去straight and level (太aggressive 嘅control input 可能會有 secondary stall)~