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In this diagram, the red team is executing a left wing lock. The left wing lock is a defensive ice hockey strategy similar to the neutral zone trap. In the most basic form, once puck possession changes, the left wing moves back in line with the defencemen. Each defender (including the left winger) plays a zone defence and is responsible for a ...
Numbered 13, [notes 4] the loose forward or lock forward packs behind the two-second-rows in the scrum. Some teams choose to simply deploy a third prop in the loose forward position, while other teams use a more skilful player as an additional playmaker.
The locks form the second row, with the loosehead lock (number 4) on the left and the tighthead lock (number 5) on the right. They scrummage by pushing against the front row, thereby providing much of the power, and are commonly known as the engine room. [ 23 ]
In this diagram, the red team is executing a neutral zone trap resulting in the blue team dumping the puck in. The neutral zone trap (often referred to as simply the trap) is a defensive strategy used in ice hockey to prevent an opposing team from proceeding through the neutral zone (the area between the blue lines) and to force turnovers.
The original Grind Line in Detroit consisted of Kris Draper, Joe Kocur, and Kirk Maltby, during the Red Wings' heyday in the late-1990s. [2] Draper played the centre position and was known for his speed and ability to win face-offs.
Left foot forward, left side leading Facing line of dance: Toe & (1 ⁄ 2 beat) Right foot crosses loosely behind left foot Backing center 1 ⁄ 4 to right between 1 and "&" Toe 2 Left foot to side and slightly back Backing diagonal center 1 ⁄ 8 between "&" and 2 Toe 3 Right foot to side in PP, having brushed towards left foot
A raised aileron reduces lift on that wing and a lowered one increases lift, so moving the aileron control in this way causes the left wing to drop and the right wing to rise. This causes the aircraft to roll to the left and begin to turn to the left. Centering the control returns the ailerons to the neutral position, maintaining the bank angle ...
If a swept wing is continuous - an oblique swept wing - the pressure isobars will be swept at a continuous angle from tip to tip. However, if the left and right halves are swept back equally, as is common practice, the pressure isobars on the left wing in theory will meet the pressure isobars of the right wing on the centerline at a large angle.