Based on this YouTube video's total view count of 173K views and industry-standard rates, the estimated total earning is $121 - $346 through ad revenue. Historical data is not yet available to calculate daily, weekly, or monthly averages.

Explore Chinook CH-47 Helicopter Ground Resonance Test and Self Destructs with Rear Tandem Rotor Breaking with 173,093 views, 932 likes, and 2 comments. Experience the impact of this video content that has captured audience attention.

Chinook CH-47 Helicopter Ground Resonance Test and Self Destructs with the Rear Tandem Rotor Breaking, and Causing the Destruction of the Aircraft. The following Wikipedia article extract detail he Ground Resonance condition http://en.wikipedia.org/wiki/Ground_resonance "Ground resonance is a hazardous condition that can occur any time the rotor of a helicopter or autogyro is turning while the aircraft is on the ground. Similar in concept to the behavior of a washing machine when the clothes are concentrated at one point during the spin cycle, ground resonance can occur with a rotorcraft when the spacing between blades becomes irregular or the damping system, including drag hinge dampers, landing gear oleo struts, or wheel tire pressure, is operating out of limits. Ground resonance occurs at three rotor RPM bands, the first at about one-third of normal rotor speed, the second at a range including normal rotor speed, and the last in a range above normal rotor speed. Ground resonance is precipitated by a shock to the aircraft arising from excessive motion of a rotor blade in its plane of rotation thereby moving the rotor center of gravity from the axis of rotation. Inadequate damping allows the rotor center of gravity to spiral away from the rotor axis of rotation, causing the rotor to generate unbalanced rotating moments beyond the compensating ability of the damping system. In addition to damping system malfunctions mentioned above, such blade movement can occur as a result of taxiing over rough ground with the rotor turning at a speed within a susceptible range, or takeoff/landing in which a shock occurs to one side of the landing gear."

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