One of the wings of a Cessna 172 airplane is shown. The wing is supported by a strut BE with ball-and-socket joints at B and E and by bearings at A and F. The bearings are perfectly aligned and are supported by a straight shaft which is fixed to the fuselage, and bearing A is a thrust bearing. Bearings A and Flie on the x axis, point B lies on the y axis, point Elies on the z axis, and points C and D lie in the xy plane. The plane's mass, including fuel, passengers, and cargo, is 1000 kg, and it flies so that it is in static equilibrium. The strut BE has negligible mass and the wing ABCDF has 200 kg mass with center of gravity at point B. The force Q acts in the -x direction and is due to air drag. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. 0.1 m 0.1 m 0.3 m 1.4 m x 2 m 0.6 m D Determine the resultant lift force P that this wing supports, assuming this force is vertical and that only the wings provide lift for the plane. (Round the final answer to four decimal places.) (Do not include a minus sign in your response.) The resultant lift force that the wing supports is INt.

One of the wings of a Cessna 172 airplane is shown. The wing is supported by a strut BE with ball-and-socket joints at B and E and by bearings at A and F. The bearings are perfectly aligned and are supported by a straight shaft which is fixed to the fuselage, and bearing A is a thrust bearing. Bearings A and Flie on the x axis, point B lies on the y axis, point Elies on the z axis, and points C and D lie in the xy plane. The plane's mass, including fuel, passengers, and cargo, is 1000 kg, and it flies so that it is in static equilibrium. The strut BE has negligible mass and the wing ABCDF has 200 kg mass with center of gravity at point B. The force Q acts in the -x direction and is due to air drag. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. 0.1 m 0.1 m 0.3 m 1.4 m x 2 m 0.6 m D Determine the resultant lift force P that this wing supports, assuming this force is vertical and that only the wings provide lift for the plane. (Round the final answer to four decimal places.) (Do not include a minus sign in your response.) The resultant lift force that the wing supports is INt.

International Edition---engineering Mechanics: Statics, 4th Edition

4th Edition

ISBN:9781305501607

Author:Andrew Pytel And Jaan Kiusalaas

Publisher:Andrew Pytel And Jaan Kiusalaas

Chapter4: Coplanar Equilibrium Analysis

Section: Chapter Questions

Problem 4.97P: The figure shows a wire cutter. Determine the cutting force on the wire at A when the 75-N forces...

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