How to calculate rate of tank pressure change

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Homework Help Overview

The discussion revolves around calculating the rate of change of pressure in a tank as air is pumped in at a constant rate. The subject area is aerodynamics, specifically focusing on gas laws and pressure dynamics in a controlled environment.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • Participants explore the relationship between mass flow rate and pressure change, referencing the ideal gas law and the equation of state. Some participants attempt to derive pressure from density and volume, while others suggest focusing on the conversion of mass to moles to apply the ideal gas law correctly.

Discussion Status

There is an ongoing exploration of different approaches to relate mass flow rate to pressure change. Some participants have provided guidance on focusing on the rate of change of moles, while others express uncertainty about their calculations. A participant claims to have reached a solution, but the discussion remains open with varying interpretations of the problem.

Contextual Notes

Participants are working under the constraints of a homework assignment, which may limit the information available for solving the problem. There is a mention of specific constants and conversions relevant to the calculations, but no definitive conclusions have been reached by all participants.

Alfredo78
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Hello everyone,
I'm new to the forum and after doing a basic search I wasn't able to find anything that would help me with a particular problem. I'm taking an online Aerodynamics course with Embry-Riddle and I can't figure out how to solve the following:


Homework Statement




If air is being pumped into a 10 ft^3 tank at a rate of 0.01 lbm/sec, and the tank temperature is being held constant at 70 F. How fast (lb/ft^2/sec) is the pressure in the tank rising?

Homework Equations



Equation of state (pressure = density*specific gas constant*temperature)
dp/dt=dM/dt * RT/V (or something like that)

The Attempt at a Solution



I tried to get things going by solving for pressure with standard sea-level density then finding the mass (mass= density*volume) but...then I just get lost.


Any help would be greatly appreciated. Thanks

Al
 
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Alfredo78 said:
Hello everyone,
I'm new to the forum and after doing a basic search I wasn't able to find anything that would help me with a particular problem. I'm taking an online Aerodynamics course with Embry-Riddle and I can't figure out how to solve the following:


Homework Statement




If air is being pumped into a 10 ft^3 tank at a rate of 0.01 lbm/sec, and the tank temperature is being held constant at 70 F. How fast (lb/ft^2/sec) is the pressure in the tank rising?

Homework Equations



Equation of state (pressure = density*specific gas constant*temperature)
dp/dt=dM/dt * RT/V (or something like that)

The Attempt at a Solution



I tried to get things going by solving for pressure with standard sea-level density then finding the mass (mass= density*volume) but...then I just get lost.

It looks like you are on the right track.

PV = NRT

V and T are being held constant. R is a constant so all you need to translate is the rate that Pressure changes (dP/dt time not temp) consistent with the change in lbs of air / sec. You need to relate the given change in lbs of air to the change in N which is the number of moles of air to satisfy the ideal Gas Law.

This yields your dP/dt = dN/dt * RT/V

Make sure your units are correct.
 
So...If 0.01 is my mass rate of change...

P=NRT= (2.3769*10^-3)(1716)(530)=2161.74

and Mass= density*volume = 2.3769*10^-2 slugs * 10ft^3

multiplied by weight of air, 32.2=.765 lbm

then multiplied by mass rate of change .01 lbm/sec = .00765 lbm/sec

then...

dp/dt=dN/dt*RT/V = 0.00765 * (1716)(530)/10= 695.75?

I feel like I'm missing something:confused:
 
Alfredo78 said:
So...If 0.01 is my mass rate of change...

P=NRT= (2.3769*10^-3)(1716)(530)=2161.74

and Mass= density*volume = 2.3769*10^-2 slugs * 10ft^3

multiplied by weight of air, 32.2=.765 lbm

then multiplied by mass rate of change .01 lbm/sec = .00765 lbm/sec

then...

dp/dt=dN/dt*RT/V = 0.00765 * (1716)(530)/10= 695.75?

I feel like I'm missing something:confused:

Careful. I don't think density is quite the right approach. I'd suggest focusing on the rate of change of mass. What you are looking for is Moles to satisfy the Perfect Gas Law equation. What you are given is mass as a rate of change. Convert mass to moles. I believe that it is the rate of change of moles that gives you your rate of change of Pressure scaled by the effect of the other constants in the relation.

Perhaps this helps:
WikiPedia said:
The mean molar mass of air is 28.97 g/mol.
http://en.wikipedia.org/wiki/Earth's_atmosphere

Of course that's grams per Mole, but you can convert.
 
Last edited:
Also at the same link I see:

R = 53.34 ft·lbf·°R−1·lbm−1 (for air)
 
LowlyPion said:
Also at the same link I see:

Thanks for the help! I finally figured it out. The answer is 28.24 lb/ft^2/sec!
 
Alfredo78 said:
Thanks for the help! I finally figured it out. The answer is 28.24 lb/ft^2/sec!

I didn't calculate anything. I will defer to your arithmetic.

Hopefully, so will your grader.

Cheers.
 

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