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marshall27 [118]
3 years ago
14

An Otto cycle with air as the working fluid has a compression ratio of 8.2. Under cold air standard conditions, what is the ther

mal efficiency of this cycle?
Engineering
1 answer:
Tresset [83]3 years ago
5 0

Answer:

Under cold air standard conditions, the thermal efficiency of this cycle is 56.9 percent.

Explanation:

From Thermodynamics we remember that thermal efficiency of the ideal Otto cycle (\eta_{th}), dimensionless, is defined by the following formula:

\eta_{th} = 1-\frac{1}{r^{\gamma-1}} (Eq. 1)

Where:

r - Compression ratio, dimensionless.

\gamma - Specific heat ratio, dimensionless.

Please notice that specific heat ratio under cold air standard conditions is \gamma = 1.4.

If we know that r = 8.2 and \gamma = 1.4, then thermal efficiency of the ideal Otto cycle is:

\eta_{th} = 1-\frac{1}{8.2^{1.4-1}}

\eta_{th} = 0.569

Under cold air standard conditions, the thermal efficiency of this cycle is 56.9 percent.

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Race cars at the Indianapolis Speedway average speeds of 185 mi/h. After determining the altitude of Indianapolis, find the Mach
denis23 [38]

Answer:

- the Mach number is 0.24.

- Compressibility becomes effective when Mach number is greater than 0.3, the Mach number of the race cars is less than 0.3, hence, compressibility will not affect their aerodynamics.

Explanation:

Given the data in the question;

Average speed V = 185 miles per hour = ( 185 /2.237 ) m/s = 82.7 m/s

From Almanac, we can find that Indianapolis is at 220 m altitude.

So from table, at that altitude, the standard speed of sound will be 339.4 m/s .

Mach number of the race car will be;

Mach Number = Velocity / sound speed

we substitute

Mach Number = ( 82.7 m/s ) / ( 339.4 m/s )

Mach Number = 0.24

Therefore the Mach number is 0.24.

We know that, compressibility becomes effective when the Mach number is greater than 0.3.

Since the Mach number of the race cars is less than 0.3, compressibility will not affect their aerodynamics.

 

8 0
3 years ago
it is used to meusure the amount of electric current. A.clamp meter. B .micrometer C steel rule D. electric meter​
Marianna [84]

Answer:

<em>Option D </em>

<em>Electric meter is used to </em><em>measure</em><em> the amount of electric current</em>

6 0
3 years ago
A simple formula to estimate the upward velocity of a rocket (neglecting the aerodynamic drag) is:
Bingel [31]

Answer:

Test code:

>>u=10;

>>g=9.8;

>>q=100;

>>m0=100;

>>vstar=10;

>>tstar=fzero_rocket_example(u, g, q, m0, vstar)

Explanation:

See attached image

5 0
3 years ago
A rigid canister with a radius of 5 in and a height of 10 in is filled with air. The initial pressure and temperature of air in
Elza [17]

Answer:1.458 Btu

Explanation:

Given

radius of canister\left ( r\right )=5in

Height of canister\left ( h\right )=10 in.

Initial pressure\left ( P_i\right )=14.7 Psi

Initia ltemprature\left ( T_i\right )=70^{\circ}F

Final pressure\left ( P_f\right )=30Psi

as canister is rigid therefore change in volume is zero

therefore

\frac{P_i}{T_i}=\frac{P_f}{T_f}

\frac{14.7}{70}=\frac{30}{T_f}

T_f=142.85^{\circ}F

volume of canister=\pi \times r^{2}\times h

                               =\pi \times 5^{2}\times 10=250\pi

volume of canister=12872,038.8 mm^3

now calculating mass of air

PV=mRT

substituting values

\left ( 14.7Psi\right )\left ( 12872,038.8 mm^3\right )=m\left ( 0.287\right )\left ( 70^{\circ}F\right )

m=21.0192 gm

Therefore heat transferred =mc_p\left ( T_f-T_i\right )

                                             =21.0192\times 10^{-3}\times \left ( 142.857-70\right )

                                             =1539.052J=1.458Btu

3 0
4 years ago
If you are unsure about holding a piece of wood to be drilled, then you should always use a
alisha [4.7K]
C I took construction class
4 0
3 years ago
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