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Consider the venturi tube of Problem and Figure without the manometer. Let A equal 5a. Suppose the pressure pt at A is 2.0 atm. Compute the values of
(a) The speed V at A and
(b) The speed v at that makes the pressure p2 at an equal to zero.
(c) Compute the corresponding volume flow rate if the diameter at A is 5.0 cm. The phenomenon that occurs at a when p2 falls to nearly zero is known as cavitations. The water vaporizes into smallbubbles.
1.49 kilograms of water in a container have pressure of 200 kpa and temperature of 500 celsius. What is the volume of this container? Round to 3 decimal places and v must be in m^3
The flow around a model of a turbine blade is investigated. The model is five times larger than the prototype. A maximum pressure of 4 psi is measured at the leading edge, a maximum velocity of fps is measured near the top of the blade, and a small d..
a steady flow compressor is used to compress air from 1 atm 25ordmc to 8 atm in an adiabatic process. the compressor
a rocket is launched from the ground in vertical direction. but its engine failed at the moment the rocket has reached
hot water at 60 c enters a thin copper tube with an inside dia of 6mm and a length of 20m. the copper tube is exposed
the outer surface of a spacecraft has an emissivity of 0.8 and an absorptivity of 0.3 for solar radiation. if solar
Describe on your own words the three strengthen mechanism for metals (i.e. grain size reduction, solid solution strengthening and strain hardening). Be sure to explain how dislocations are involved in each of the strengthening techniques.
a new dam project will require 48000 a year in maintenance costs after it is complete. these maintenance costs will
How to estimate polygon point 1? Hw6 have used shmin = (sv - pp)/3.1 + pp. Where sv = 1.1 and pp = 0.5.
fig book design of machinerywith using the following data for the above diagram find torque at o2 and forces at o2 a
in the system below for measuring fluid viscosity the inner cylindrical core is stationary the outer cylindrical shell
Derive an expression for lift co-efficient of a Van de Vooren Airfoil having chord length =2l,thickness parameter E and trailing angle tau. Discuss the effects of E and tau on the lift of Van De Vooren Airfoil.
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