Questions
Use MATLAB to determine the intersection point for the sets of equations shown below.

Use MATLAB to determine the intersection point for the sets of equations shown below. Use the backslash when possible.Graph the equations with different colors, and plot the intersection point with a red star marker. If the equations do not intersect, graph them anyway.

Include a legend:

a) -4x1 + 2x2 = 10                                                                                b)-4x1+2x2^3 = 10

x1 + x2 = -8                                                                                           x1+ x2 = -8                   

In: Mechanical Engineering

What are the other components that can improve the COP. Draw the P-h diagram to explain...

What are the other components that can improve the COP. Draw the P-h diagram to explain the process.

In: Mechanical Engineering

What is the principle operation of the evaporator?

What is the principle operation of the evaporator?

In: Mechanical Engineering

How do the condensers reject heat?

How do the condensers reject heat?

In: Mechanical Engineering

Alloy element content has an effect on the ductile-to-brittle transition temperature of a steel. How does...

Alloy element content has an effect on the ductile-to-brittle transition temperature of a steel. How does increasing the Mn content of a steel affect the transition temperature?

In: Mechanical Engineering

Considering the nature of the Charpy impact test can the impact energy values obtained from it...

Considering the nature of the Charpy impact test can the impact energy values obtained from it be used directly in mechanical design? Explain your answer. ?

In: Mechanical Engineering

1. Aerodynamics : (a) how to find zero lift line of a wing and airfoil?

[Aerospace Engineering]

1. Aerodynamics :

(a) how to find zero lift line of a wing and airfoil?

(b) how do we relate this with climb angle(gamma), pitch angle(theta), angle of incidence, and Angle of Attack(Alpha)

(c) why during climb Theta is not considered as Angle of attack since the aircraft moves with respect to x-axis? or is that with respect to thrust direction?

(d) then can we classify Angle of Attack to be similar with Angle of Incidence if the aircraft flies along the direction of thrust?

2. Flight Mechanics :

a) what is the differences between stick-fixed and stick-free? (including explanation on each)

b) consider that the aircraft flies in autopilot mode, is that considered as stick-fixed,free, or neither?

c) Consider Horizontal stabiliser on conventional aircraft, how to find these variables? given

C_LT = 2*phi*Alpha_Teffective + a2(eta) +a3(beta), ; C_LT is known, Aileron hinge location x1/c = 0.65 and Trim Tab hinge at x2/c = 0.8

C_H = b1*Alpha_Teffective + b2(eta) + a2(beta), ;beta = Trim tab deflection angle; eta = Elevator deflection angle

 

In: Mechanical Engineering

A boiler produces steam at a saturated temperature of 300C and at dryness of 92% from...

A boiler produces steam at a saturated temperature of 300C and at dryness of 92% from feedwater at 110C The boiler evaporating rate is 70 kg min. What is boiler heat rate ?

The density of steam at pressure 1.100 kPa is ?

In: Mechanical Engineering

For a brass alloy, the tensile strength is 400 MPa, the yield strength is 315 MPa...

For a brass alloy, the tensile strength is 400 MPa, the yield strength is 315 MPa and the modulus of elasticity is 100 GPa.

(a) What is the maximum load that may applied to the specimen with a cross sectional area of 130 mm2 before it fractures?

(b) For the same cross sectional area, if the original length of the specimen is 75 mm what will be the length of the specimen, when a load of 13000 N is applied in the longitudinal direction?

In: Mechanical Engineering

Consider a pipe (diameter of 50 mm) with air flowing through it. The inlet conditions are:...

Consider a pipe (diameter of 50 mm) with air flowing through it. The inlet conditions are: Mach 3; total pressure = 1000 kPa and 550 K. The friction coefficient (f) is 0.004. The exit Mach number decreases with the length of the pipe. Assume adiabatic, steady flow.

Write a short Matlab code and plot the following, while the exit Mach number changes from 2.5 to 0.99 with increments of ?M=0.01. Find the length of the pipe that is going to give the desired exit Mach number. Find the pipe exit pressure, pipe exit temperature, and pipe exit total pressure.

In: Mechanical Engineering

what happens to cutting force as the following increase: a.Rake angle b.Material shear strength c.Depth of...

what happens to cutting force as the following increase: a.Rake angle b.Material shear strength c.Depth of cut Are your findings as expected based on the theory of machining? Why or why not?

In: Mechanical Engineering

Name three professions related to kinesiology and explain how each will benefit from a knowledge of...

Name three professions related to kinesiology and explain how each will benefit from a knowledge of biomechanics.

In: Mechanical Engineering

How much energy does it require to keep the ice steady at -8 degrees celsius continuously?...

How much energy does it require to keep the ice steady at -8 degrees celsius continuously?

We have an ice rink and these are the values:

- indoor climate has a constant temperature of +10 degree celsius

- It took 17669880 KJ to cool it down from +10 celcius to -8 celcius.

- Dimensions 60m length x 30m width x 2.5cm thickness, which is 45 cubic meter of ice

How much energy is needed to keep the rink cooled down at -8 degrees per hour?

In: Mechanical Engineering

Which of the following is least likely to decrease the thermal contact resistance between two media...

Which of the following is least likely to decrease the thermal contact resistance between two media in contact?

Make a vacuum gap at the interface

Apply thermal grease onto the interface

Sand the contact surface smooth

Apply pressure one against another

In: Mechanical Engineering

What are uniform pressure and uniform wear theories? Deduce expressions for the friction torque considering both...

What are uniform pressure and uniform wear theories? Deduce expressions for the friction torque considering both the theories for a flat collar.

In: Mechanical Engineering