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juin [17]
4 years ago
9

A walrus loses heat by conduction through its blubber at the rate of 220 W when immersed in −1.00°C water. Its internal core tem

perature is 37.0°C, and it has a surface area of 2.23 m2. What is the average thickness of its blubber? The conductivity of fatty tissue without blood is 0.20 (J/s · m · °C).
Engineering
1 answer:
Llana [10]4 years ago
7 0

Answer:

The average thickness of the blubber is<u> 0.077 m</u>

Explanation:

Here, we want to calculate the average thickness of the Walrus blubber.

We employ a mathematical formula to calculate this;

The rate of heat transfer(H) through the Walrus blubber = dQ/dT = KA(T2-T1)/L

Where dQ is the change in amount of heat transferred

dT is the temperature gradient(change in temperature) i.e T2-T1

dQ/dT = 220 W

K is the conductivity of fatty tissue without blood = 0.20 (J/s · m · °C)

A is the surface area which is 2.23 m^2

T2 = 37.0 °C

T1 = -1.0 °C

L is ?

We can rewrite the equation in terms of L as follows;

L × dQ/dT = KA(T2-T1)

L = KA(T2-T1) ÷ dQ/dT

Imputing the values listed above;

L = (0.2 * 2.23)(37-(-1))/220

L = (0.2 * 2.23 * 38)/220 = 16.948/220 = 0.077 m

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brilliants [131]

Answer:

the kilogram (kg), for mass.

the second (s), for time.

the kelvin (K), for temperature.

the ampere (A), for electric current.

the mole (mol), for the amount of a substance.

the candela (cd), for luminous intensity.

the meter (m), for distance.

Explanation:hoped this helped

6 0
3 years ago
Read 2 more answers
Pineapple contains about 20 wt% solid and the balance water. To make pineapple jam, crush
Allisa [31]

The system is exactly, specified problem and the values of all the unknows will be determined unkowns will have a unique value.

<u>Explanation:</u>

given informtion:

pineapple:

water = 80 % = 0.8

solids = 20% = 0.2

pineapple : sugar = 1:5

jam:

water = 30% = 0.3

solids and sugar = 70%

basis: 1 kg pineapple

therefore, sugar = 5 kg

the process flow sheet is as:

As per the figures shown in the attached file, DOF = 0, thus the system is exactly, specified problem and the values of all the unknows will be determined unkowns will have a unique value.

8 0
3 years ago
Around the 1760s what allowed for more supplies to be moved around?
Licemer1 [7]

Around the 1760s the factor that allowed for more supplies to be moved around<u>-A free trade agreement</u>

<u />

Explanation:

A free trade agreement is a contract between two or more countries  to reduce the export and import  barriers . As per the  free trade agreement the  goods and services of a nation can be  bought and sold across international borders of other countries  and the  restriction imposed by the government (Like  tariffs, quotas, subsidies ) is restricted /limited in order to encourage free trade.

<u>The canton system of china is an example </u>

So the statement that Around the 1760s the factor that allowed for more supplies to be moved around<u>-A free trade agreement</u>

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3 0
3 years ago
The Boeing 787 Dreamliner is billed to be 20% more fuel efficient than the comparable Boeing 767 and will fly at Mach 0.85. The
evablogger [386]

Answer:

the projected volumetric flow rate of fuel for each of the two Dreamliner engines is 0.005 m³/s

Explanation:

Given the data in the question;

First we determine the fuel economy of Boeing 767

Range = 12,000 km

fuel capacity = 90,000 L

so,  fuel economy of Boeing 767 will be

η_f = Range / fuel capacity

η_f = ( 12,000 km / 90000 L ) ( 1000m / 1 km) ( 3.7854 L/gal × 264.2 gal/m² )

η_f  = 133,347.024 m/m³

Now, Boeing 787 is 20% more fuel efficient than Boeing 767

so fuel economy of Boeing 787 will be;

⇒ (1 - 20%) × fuel economy of Boeing 767

⇒ (1 - 0.2) × 133,347.024 m/m³

⇒ 0.8 × 133,347.024 m/m³

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Hence, fuel economy of Boeing 787 dream line engine is

⇒ 106,677.6 m/m³ / 2 = 53,338.8 m/m³

Next, we find the velocity of Boeing 787

V_{787 = Mach number of 787 × speed of sound

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Now, to get the Volume flow rate for each dream liner engine { Boeing 787 };

Volumetric flow rate = velocity of flight / fuel economy

we substitute

= 265.9319 m/s / 53,338.8 m/m³

= 0.0049857 ≈ 0.005 m³/s

Therefore,  the projected volumetric flow rate of fuel for each of the two Dreamliner engines is 0.005 m³/s

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3 years ago
1. Given: R= 25 , E = 100 V<br> Solve for I
Lyrx [107]

Answer:

4 amps

Explanation:

V = I*R

I / V/R

I = 100 / 25

I = 4 amps

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3 years ago
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