
(a)
The value of

Answer to Problem 4.51P
The value of
Explanation of Solution
Given information:
The value of step function is
Write the Equation of motion.
Here, acceleration is
Calculation:
Substitute
Take Laplace transform in equation (II)
Substitute
Apply partial fraction on Equation (IV).
Equate constant term of equation (V).
Equate coefficient of
Equate coefficient of
Solve equation (VI) and (VII).
Substitute
Substitute
Take inverse Laplace of Equation (VIII).
Conclusion:
The value of
(b)
The value of

Answer to Problem 4.51P
The value of
Explanation of Solution
Given information:
The value of step function is
Write the Equation of motion.
Here, acceleration is
Calculation:
Substitute
Take Laplace transform in equation (X)
Substitute
Apply partial fraction on Equation (XII).
Equate constant term of equation (XIII).
Equate coefficient of
Equate coefficient of
Substitute
Substitute
Take inverse Laplace of Equation (XVI).
Further simplifying
Conclusion:
The value of
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Chapter 4 Solutions
EBK SYSTEM DYNAMICS
- Just do Questions 7, 9, 11. Here are notes attached for reference. I prefer handwritten solutions. ONLY UPLOAD A SOLUTION IF YOU ARE SURE ABOUT THE ANSWER PLEASE.arrow_forwardThis is a tilt and rotation question. Here are notes attached for reference. I prefer handwritten solutions. ONLY UPLOAD A SOLUTION IF YOU ARE SURE ABOUT THE ANSWER PLEASE. I prefer handwritten solutions.arrow_forwardA turbine blade made of a metal alloy (k = 17 W/m-K) has a length of 5.3 cm, a perimeter of 11 cm, and a cross-sectional area of 5.13 cm². The turbine blade is exposed to hot gas from the combustion chamber at 1133°C with a convection heat transfer coefficient of 538 W/m²K. The base of the turbine blade maintains a constant temperature of 450°C and the tip is adiabatic. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Hot gas h=538 W/m²K TL E= Turbine blade k = 17 W/m-K p=11 cm, L=5.3 cm A = 5.13cm² T=450°C Determine the temperature at the tip of the turbine blade. The temperature at the tip of the turbine blade is °C.arrow_forward
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- please find Ix in mm4arrow_forward۲/۱ ∞ + : 5V ON Date AND Loaded with an oR P 5- A R Vect bov V(22)= IR, Vcc-vd 2R V(21) V(22) + Vd=" or V(z) HomeWo Vec-T 022 51-2 العنوان Example 5.5: The turbine rotor of a ship has a mass of 30 tons, a radius of gyration of 600 mm and rotates at 2400 rpm in a clockwise direction when viewed from aft. The ship pitches through a total angle of 15%, 7.5° above and 7.5° below the horizontal, the motion being simple harmonic and having a period of 12 sec. Determine the maximum gyroscopic couple on the holding down bolts of the turbine and the direction of yaw as the Dow rises. Vezi b) V225 V22 lo 21.5 2.15 U 5-0.7 K Loka (I= Vecond R 5:4.57 U 25-0-7 Tak R 5-0.7 5kr V2, Va-IR=5-2.15 -2-85 NEW G C 'WR к >arrow_forward: + ♡ +① العنوان I need a detailed drawing with explanation so A 4 ined sove in peaper 96252 Example 5.5 The turbine rotor of ship has a mass of 30 tons, a radius of gyration of 600 mm and rotates at 2400 rpm ia clockwise direction when viewed from aft. The ship pitches through a total angle of 7.5° above and 7.5° below the horizontal, the motion beingle harmonic and hav gyroscopic couple on the bow rises. ding down be a period of 12 sec. Determine the maximum of the turbine and the direction of yaw as bax r 2.01 ۳/۱arrow_forward
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