Answer:
See explaination and attachment.
Explanation:
Iteration method is a repetitive method applied until the desired result is achieved.
Let the given equation be f(x) = 0 and the value of x to be determined. By using the Iteration method you can find the roots of the equation. To find the root of the equation first we have to write equation like below
x = pi(x)
Let x=x0 be an initial approximation of the required root α then the first approximation x1 is given by x1 = pi(x0).
Similarly for second, thrid and so on. approximation
x2 = pi(x1)
x3 = pi(x2)
x4 = pi(x3)
xn = pi(xn-1).
please go to attachment for the step by step solution.
Answer:
2021 super star wagon master
Technician a is correct because he says that Many common rail injectors filters can be bypassed by dirt, which can lead to an injector sticking open and continuously fueling a cylinder.
Coalescence is used to separate the water and fuel. To the fuel injector cleaning kit, fasten your air compressor. Diesel engines run at compression ratios that are greater than those of gasoline engines. greater ratio compared to gasoline engines. increased thermal expansion as a result. more fuel energy that is transformed into usable power. The great benefit of using a dry cylinder sleeve is that by quickly installing new sleeves, the cylinder block can be quickly restored to its original specifications. Vacuum drying can be used to get rid of small amounts of water. A nozzle is used to spray the fuel into the vacuum chamber of engines. Air and unsolved free water are taken out of the oil. The fuel is evenly dispersed, which facilitates efficient drying.
Learn more about injectors here:
brainly.com/question/27969202
#SPJ4
Answer:
(B) dimensions, tolerances, materials, and finishes of a component.
Explanation:
An engineering drawing :
An engineering drawing is a technical drawing which draws the actual component .
An engineering drawing shows
1. Materials
2.Dimensions
3.Tolerance
4.Finishes of a component
Engineering drawing does not shows any information about the cost of component.
So the option B is correct.
Answer:
The answer is "
"
Explanation:
Given data:
Initial temperature of tank 
Initial pressure of tank 
Diameter of throat 
Mach number at exit 
In point a:
calculating the throat area:
Since, the Mach number at throat is approximately half the Mach number at exit.
Calculate the Mach number at throat.
Calculate the exit area using isentropic flow equation.
Here: 
is the specific heat ratio. Substitute the values in above equation.
exit diameter is 3.74 cm
In point b:
Calculate the temperature at throat.
Calculate the velocity at exit.
Here: R is the gas constant.
Calculate the density of air at inlet
Calculate the density of air at throat using isentropic flow equation.
Calculate the mass flow rate.
