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 bow rises.

Two cylinders rolling in the opposite direction has a speed ratio of 3. If the diameter of driver is 10 inches, find the center distance between cylinders. A. 15 in B. 10 in C. 25 in. D. 20 in. Please solve the Problem elaborately. Your solution will be use as reference for my studies. Thank you so much your work will be appreciated much!

L + ined sove in peaper X-P 96852 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 bow rises. -20125 750 x2.01

The mass of a propeller is 4.5 tons and its centre of gravity is 3.5 mm from the centre of rotation. Find the pull due to centrifugal force when it is rotating at 120 rev/min.

: + ♡ +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 ۳/۱

i need the answer quickly

2. A symmetric spacecraft is separated from a Delta II launch vehicle which is spinning at 30 RPM. If the separation system imparts a small angular transverse rate of 2%sec at the instant of separation, calculate the nutation angle for a spacecraft roll-to-pitch ratio of 0.5.

question 2 A mass ! hangs on the end of a cord around a pulley of radius 5 and moment of inertia 6, rotating with an angular velocity ,, as shown in the figure below. The rim of the pulley is attached to a spring (with constant 7). Assume small oscillations so that the spring remains essentially horizontal and neglect friction so that the conservation of energy of the system yields: 1 2 !91 + 1 2 6,1 + 1 2 7;1 − !); = =, ?ℎABA , = 9 5 , = = CDE&/, ; = FG&H'5CA!AE/ IBD! AJ(G'GKBG(! Find the natural circular frequency of the system in terms of !, 5, 7,6, and ).

An aeroplane makes a complete half circle of 50 metres radius, towards left, when flying at 200 km per hour. The rotary engine and the propeller of the plane has a mass of 400 kg with a radius of gyration of 300 mm. The engine runs at 2400 r.p.m. clockwise, when viewed from the rear. Find the gyroscopic couple on the aircraft and state its effect on it. What will be the effect, if the aeroplane turns to its right instead of to the left ?

Estimate the period T of a kitchen broom allowed to swing in small oscillations while suspended from the end of the handle. The oscillating broom is a physical pendulum. Start by considering the different parts that make up a broom. Think of their shapes and sizes and make estimations for their masses, lengths, and moments of inertia.