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Problem 11.013 - Velocity and acceleration vector components in two distinct reference frames At the instant shown, when expressed via the (ut, un) component system, the airplane's velocity and acceleration are (140ût) m/s and a = (–7.25ût +182ũn) m/s². Determine the angle between the velocity and acceleration vectors. In addition, treating the (ut, ûn) and (î, 3) component systems as stationary relative to one another, express the airplane's velocity and acceleration in the (î, 3) component system. (Include a minus sign if necessary.) V = $ ûn U₂ The angle is 87.72 °. (Round the final answer to four decimal places.) The airplane's velocity in the (1, 3) component system is =([ decimal places.) The airplane's acceleration in the (î, 3) component system is a =(| decimal places.) + j) m/s. (Round the final answers to four 3) m/s2. (Round the final answer to two

Problem 11.013 - Velocity and acceleration vector components in two distinct reference frames At the instant shown, when expressed via the (ut, un) component system, the airplane's velocity and acceleration are (140ût) m/s and a = (–7.25ût +182ũn) m/s². Determine the angle between the velocity and acceleration vectors. In addition, treating the (ut, ûn) and (î, 3) component systems as stationary relative to one another, express the airplane's velocity and acceleration in the (î, 3) component system. (Include a minus sign if necessary.) V = $ ûn U₂ The angle is 87.72 °. (Round the final answer to four decimal places.) The airplane's velocity in the (1, 3) component system is =([ decimal places.) The airplane's acceleration in the (î, 3) component system is a =(| decimal places.) + j) m/s. (Round the final answers to four 3) m/s2. (Round the final answer to two

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Problem 11.013 - Velocity and acceleration vector components in two distinct reference frames At the instant shown, when expressed via the (ut, ûn) component system, the airplane's velocity and acceleration are V = = (140ût) m/s and a = (–7.25ût + 182ũn) m/s². Determine the angle between the velocity and acceleration vectors. In addition, treating the (ût, ûn) and (î, 3) component systems as stationary relative to one another, express the airplane's velocity and acceleration in the (î, î) component system. (Include a minus sign if necessary.) 4 57° in The angle is 87.72°. (Round the final answer to four decimal places.) The airplane's velocity in the (i, i) component system is = (| decimal places.) The airplane's acceleration in the decimal places.) (i, i) component system is a = (| 3) m/s. (Round the final answers to four j) m/s2. (Round the final answer to two
Transcribed Image Text:Problem 11.013 - Velocity and acceleration vector components in two distinct reference frames At the instant shown, when expressed via the (ut, ûn) component system, the airplane's velocity and acceleration are V = = (140ût) m/s and a = (–7.25ût + 182ũn) m/s². Determine the angle between the velocity and acceleration vectors. In addition, treating the (ût, ûn) and (î, 3) component systems as stationary relative to one another, express the airplane's velocity and acceleration in the (î, î) component system. (Include a minus sign if necessary.) 4 57° in The angle is 87.72°. (Round the final answer to four decimal places.) The airplane's velocity in the (i, i) component system is = (| decimal places.) The airplane's acceleration in the decimal places.) (i, i) component system is a = (| 3) m/s. (Round the final answers to four j) m/s2. (Round the final answer to two
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