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In a Pelton-wheel turbine, a stream of water is deflected by a series of blades so that the rate at which water is deflected by the blades is equal to the rate at which water issues from the nozzle
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Vector Mechanics for Engineers: Dynamics
- A launch vehicle has 6 engines operating in parallel which are fed from the same propellant tank. Initially, each engine has an equivalent exhaust velocity of 3500 m/s and consumes 400 kilograms of propellant per second. One of the engines malfunctions and consequently operates at 50% thrust and 120% propellant consumption. Calculate the equivalent exhaust velocity in m/s of all engines if treated as a single engine, including the malfunctioning engine in your calculation.arrow_forwardA pump draws water from a reservoir A and lifts it to reservoir B. The loss of head from A to point 1 is 3 times the velocity head in the 150 mm pipe and the loss of head from point 2 to B is 25 times the velocity head in the 100 mm pipe. When reservoir A is a starting point at elevation 0 and connected to point 1, where point 1 is also connected with a pump and point 2 is at elevation 20 m. which is connected with a pump that travels to reservoir B at elevation of 240 m. The discharge is 25 liters/sec, compute the pressure head at point 1. a. 268 m b. 134 m c. 19.74 m d. 39.48 marrow_forwardConsider an airplane with a jet engine attached to the tail section that expels combustion gases at a rate of 18 kg/s with a velocity of V = 300 m/s relative to the plane. During landing, a thrust reverser (which serves as a brake for the aircraft and facilitates landing on a short runway) is lowered in the path of the exhaust jet, which deflects the exhaust from rearward to 120°. Determine (a) the thrust (forward force) that the engine produces prior to the insertion of the thrust reverser and (b) the braking force produced after the thrust reverser is deployed.arrow_forward
- Consider an airplane with a jet engine attached to the tail section that expels combustion gases at a rate of 18 kg/s with a velocity of V = 300 m/s relative to the plane. During landing, a thrust reverser (which serves as a brake for the aircraft and facilitates landing on a short runway) is lowered in the path of the exhaust jet, which deflects the exhaust from rearward to 150°. Determine (a) the thrust (forward force) that the engine produces prior to the insertion of the thrust reverser and (b) the braking force produced after the thrust reverser is deployed.arrow_forward43. A 30ft x 5ft diameter storage tank containing water at its maximum level is being drained by a drain valve located at the bottom of the tank. It was seen that the velocity of exit water changes as the height of the water level in the tank. At the instant the water level is at 10Oft from the bottom of the tank, determine the instantaneous time required to empty the tank if the drain pipe diameter is 25mm. a. 24.7184mins. b. 25.7277mins. c. 22.5647mins. d. 24.4060mins.arrow_forwardA jet of water from a nozzle is deflected through an angle θ = 60° from its original direction by a curved vane which it enters tangentially (see Fig. 5.5) without shock with a mean velocity C1 of 30 m s−1 and leaves with a mean velocity C2 of 25 m s−1. If the discharge A from the nozzle is 0.8 kg s−1, calculate the magnitude and direction of the resultant force on the vane if the vane is stationary.arrow_forward
- 5. A 60-kg ice skater is standing on ice with ice skates (negligible friction). She is holding a flexible hose (essentially weightless) that directs a 2-cm-diameter stream of water horizontally parallel to her skates. The water velocity at the hose outlet is 10 m/s relative to the skater. If she is initially standing still, determine: (a) the velocity of the skater and the distance she travels in 5 s., (b) how long it will take to move 5 m and the velocity at that moment. Ice skater 10 m/s D = 2 cmarrow_forwardProblem 1. A liquid-fueled rocket motor consumes 80 kg/s of nitric acid as oxidizer and 32 kg/s of aniline as fuel while being tested at its rated design conditions. The products of combustion leave axially at an average velocity of 180 m/s relative to the rocket nozzle and at an absolute pressure of 110 kPa. The nozzle exit diameter is 0.60 m. Calculate the thrust produced by the rocket motor on the test stand while operating at standard sea-level pressure.arrow_forwardA jet strikes a stationery curved vane without shock and is deflected 150° from its original direction. The discharge from the jet is 0.68kg/s and the velocity is 24m/s. Assume that there is no reduction of relative velocity due to friction and determine the magnitude and direction of thearrow_forward
- A pump is located near the edge of the horizontal platform shown. The nozzle at A discharges water with an initial velocity of 24 ft/s at an angle of 55° with the vertical. Determine the range of values of the height h for which the water enters the opening BC. The range of values of h is _____ ft < h < _____ ft.arrow_forwardCalculate the kinetic energy of a body of mass m moving with velocity u or the rate of transport of kinetic energy by a stream moving with mass flow rate m_ and velocity u. Calculate the gravitational potential energy of a body of mass m at elevation z or the rate of transport of gravitational potential energy by a stream moving with mass flow rate m_ at elevation z, where zis height above a reference plane at which potential energy is defined to equal zero.arrow_forwardA stream of water flowing at a rate of 1.2 m3/min and moving with a speed of 30 m/s at both A and B is deflected by a vane welded to a hinged plate. Knowing that the combined mass of the vane and plate is 20 kg with the mass center at point G , determine (a) the angle 0, (b) the reaction at C.arrow_forward
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