The helicopter below features a pair of counter-rotating rotors that provide stability and lift. The forces FÅ and FÅ lie in the xy plane, and α and a represent angles about the z-axis. The helicopter's engine thrust produces forces Fc and Fp, whose lines of action act in the y direction. Forces QA and QB are lift forces developed by the rotors, which act in the z-direction. Moments MA and M³ result from the rotation of the rotors and are directed in the ±z direction, as shown. Points A, B, C, and D are located 2 on the lines of action of the given forces and moments. Note that point D is located on the opposite side of the helicopter and is not visible in the figure. Based on A, B, C, and D coordinates, the angles a and ağ, and magnitudes of the forces and moments listed below, compute an equivalent force system acting at the origin of the coordinate system, point O.
The helicopter below features a pair of counter-rotating rotors that provide stability and lift. The forces FÅ and FÅ lie in the xy plane, and α and a represent angles about the z-axis. The helicopter's engine thrust produces forces Fc and Fp, whose lines of action act in the y direction. Forces QA and QB are lift forces developed by the rotors, which act in the z-direction. Moments MA and M³ result from the rotation of the rotors and are directed in the ±z direction, as shown. Points A, B, C, and D are located 2 on the lines of action of the given forces and moments. Note that point D is located on the opposite side of the helicopter and is not visible in the figure. Based on A, B, C, and D coordinates, the angles a and ağ, and magnitudes of the forces and moments listed below, compute an equivalent force system acting at the origin of the coordinate system, point O.
International Edition---engineering Mechanics: Statics, 4th Edition
4th Edition
ISBN:9781305501607
Author:Andrew Pytel And Jaan Kiusalaas
Publisher:Andrew Pytel And Jaan Kiusalaas
Chapter6: Beams And Cables
Section: Chapter Questions
Problem 6.6P: Find the internal force systems acting on sections 1 and 2.
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