Answer
Given,
Reservoir pressure of a supersonic wind tunnel = 5 atm
Local Mach number = ?
Area ration = ?
a) 4 atm.
Pressure ratio =
= 0.8
From Isentropic Flow Tables
M = 0.58 A/A* = 1.213
b) 2.64 atm
Pressure ratio =
= 0.528
From Isentropic Flow Tables
M = 1 A/A* = 1
c) 0.5 atm
Pressure ratio =
= 0.1
From Isentropic Flow Tables
M =2.10 A/A* = 1.8369
Answer:
an attachment is below
Explanation:
1) the formula for damping coefficient id for RLC series circuit.
For \xi =0 you can make c=0 but inductor will still have some capacitance.
2) the responses of critically damped system and under damped system are shown with comments on their time response.
4) There can be many different answers to this question, but the 4 I have mentioned are the most important parameters we need to know about an unknown op-amp if we are to use it in our circuit.
Hope it answers all your questions.
Answer:
The change in specific internal energy is 3.5 kj.
Explanation:
Step1
Given:
Total change in energy is 15.5 kj.
Change in kinetic energy is –3.5 kj.
Change in potential energy is 0 kj.
Mass is 5.4 kg.
Step2
Calculation:
Change in internal energy is calculated as follows:
kj.
Step3
Specific internal energy is calculated as follows:
kj/kg.
Thus, the change in specific internal energy is 3.5 kj/kg.
Answer:
a)Q=131.1 MJ
b)Q=54 MJ
Explanation:
Given that
Mass ,m=200 kg
Specific heat Cp=0.46 J/g°C
Cp=0.46 KJ/kg°C
Heat of fusion = 270 J/g
Heat of fusion = 270 KJ/kg
Melting point temperature = 1450°C
a)
Initial temperature = 25°C
Final temperature=1450°C
Heat required to rise temperature from 25°C to 1450°C.
Q= m CpΔT
Q=200 x 0.46 x (1450-25) KJ
Q=131,100 KJ
Q=131.1 MJ
b)
Heat required to transform from solid phase to liquid phase
Q= Mass x heat of fusion
Q=200 x 27 KJ
Q=54,000 KJ
Q=54 MJ
Answer:
critical stress required is 18.92 MPa
Explanation:
given data
specific surface energy = 1.0 J/m²
modulus of elasticity = 225 GPa
internal crack of length = 0.8 mm
solution
we get here one half length of internal crack that is
2a = 0.8 mm
so a = 0.4 mm = 0.4 × m
so we get here critical stress that is
...............1
put here value we get
=
= 18923493.9151 N/m²
= 18.92 MPa
Answer: This is EASY!
Explanation:
To make it easy, you would convert those binary numbers and to denary. And this gives:
84 104 105 115 32 105 115 32 69 65 83 89 33
Then, the denary numbers generated can be converted to ASCII code using this ASCII Table in the attachment below. And the result is: This is EASY!
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