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Concept explainers
(a)
The time interval between a maximum positive displacement and the following maximum negative displacement is
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Explanation of Solution
Given information:
The system is underdamped, the time period between two successive points is
The figure shows the underdamped system.
Figure-(1)
Write the expression amplitude of vibrations of an underdamped system..
Here, the amplitude of an underdamped system is
Differentiate Equation (I) with respect to time.
For maximum positive and negative displacement,
The maximum negative displacement occurs after a phase difference of
Calculation:
Substitute
Here, the time interval for maximum positive displacement is
Substitute
Here, the time interval for maximum negative displacement is
Substract Equation (V) and (VI).
Substitute
Conclusion:
The time interval between a maximum positive displacement and the following maximum negative displacement is
(b)
The time interval between two successive zero displacement is
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Explanation of Solution
Calculation:
Substitute
Substitute
Here, the time interval for first zero displacement is
Substitute
Here, the time interval for second zero displacement is
Substract Equation (X) from (IX).
Substitute
Conclusion:
The time interval between two successive zero displacement is
(c)
The time interval between maximum positive displacement and zero displacement is greater than
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Explanation of Solution
Calculation:
Substract Equation (V) from (IX).
The values of
Substitute
Neglect the time interval difference to be negative.
Substitute
Conclusion:
The time interval between maximum positive displacement and zero displacement is greater than
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Chapter 19 Solutions
Vector Mechanics For Engineers
- Assume a Space Launch System (Figure 1(a)) that is approximated as a cantilever undamped single degree of freedom (SDOF) system with a mass at its free end (Figure 1(b)). The cantilever is assumed to be massless. Assume a wind load that is approximated with a concentrated harmonic forcing function p(t) = posin(ωt) acting on the mass. The known properties of the SDOF and the applied forcing function are given below. • Mass of SDOF: m =120 kip/g • Acceleration of gravity: g = 386 in/sec2 • Bending sectional stiffness of SDOF: EI = 1015 lbf×in2 • Height of SDOF: h = 2000 inches • Amplitude of forcing function: po = 6 kip • Forcing frequency: f = 8 Hz Figure 1: Single-degree-of-freedom system in Problem 1. Please compute the following considering the steady-state response of the SDOF system. Do not consider the transient response unless it is explicitly stated in the question. (a) The natural circular frequency and the natural period of the SDOF. (10 points) (b) The maximum displacement of…arrow_forwardAssume a Space Launch System (Figure 1(a)) that is approximated as a cantilever undamped single degree of freedom (SDOF) system with a mass at its free end (Figure 1(b)). The cantilever is assumed to be massless. Assume a wind load that is approximated with a concentrated harmonic forcing function p(t) = posin(ωt) acting on the mass. The known properties of the SDOF and the applied forcing function are given below. • Mass of SDOF: m =120 kip/g • Acceleration of gravity: g = 386 in/sec2 • Bending sectional stiffness of SDOF: EI = 1015 lbf×in2 • Height of SDOF: h = 2000 inches • Amplitude of forcing function: po = 6 kip • Forcing frequency: f = 8 Hz Figure 1: Single-degree-of-freedom system in Problem 1. Please compute the following considering the steady-state response of the SDOF system. Do not consider the transient response unless it is explicitly stated in the question. (a) The natural circular frequency and the natural period of the SDOF. (10 points) (b) The maximum displacement of…arrow_forwardPlease solve 13 * √(2675.16)² + (63.72 + 2255,03)² = 175x106 can you explain the process for getting d seperate thank youarrow_forward
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