Calculating pressure in high altitude?

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SUMMARY

The discussion focuses on calculating pressure changes for a special operations soldier scuba diving at a depth of 20 meters in seawater and parachuting from an altitude of 7.6 kilometers. The relevant equations used are p = p0 + ρgh, where p0 is the atmospheric pressure, ρ is the density of the fluid, g is the acceleration due to gravity, and h is the height or depth. The gauge pressure at 20 meters is calculated as p1 = 2.00 x 105 Pa, while at 7.6 kilometers, it is p2 = 6.48 x 104 Pa. The change in pressure is Δp = p1 - p2 = 1.4 x 105 Pa, but the discussion reveals an error in the solution manual regarding the sign of p2, emphasizing the importance of considering atmospheric pressure.

PREREQUISITES
  • Understanding of fluid mechanics principles, particularly pressure calculations.
  • Familiarity with the equation p = p0 + ρgh.
  • Knowledge of atmospheric pressure variations with altitude.
  • Basic understanding of gauge pressure versus absolute pressure.
NEXT STEPS
  • Study the effects of altitude on atmospheric pressure using the barometric formula.
  • Learn about gauge pressure and absolute pressure distinctions in fluid mechanics.
  • Research the impact of density variations in different fluids on pressure calculations.
  • Explore real-world applications of pressure calculations in high-altitude parachuting and diving scenarios.
USEFUL FOR

This discussion is beneficial for physics students, military personnel involved in special operations, and anyone interested in fluid mechanics and pressure calculations in varying environments.

dmk90
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Homework Statement


What is the change in pressure on a special-op soldier who must scuba dive at a depth of 20 m in seawater one day and parachute at an altitude of 7.6 km the next day? Assume that the average air density within the altitude
range is 0.87 kg/m3.

Homework Equations


p=p0 + ρgh

The Attempt at a Solution


I understand how to calculate pressure using the above formula for something at the surface, but how do I apply it to a high altitude? In the solution manual, they just ignore atmospheric pressure, so I am confused. At that high altitude, doesn't it mean the person is not affected by the usual atmospheric pressure of 1 atm?
 
Physics news on Phys.org
Pressure is less at the top of the sea than at the bottom of the sea ...
we live on the bottom of a "sea of air" that's only about 8km deep.
Pressure is zero at the "top" of the atmosphere, the edge of space.
 
dmk90 said:
In the solution manual, they just ignore atmospheric pressure, so I am confused. At that high altitude, doesn't it mean the person is not affected by the usual atmospheric pressure of 1 atm?
I doubt that the solution manual ignored the atmospheric pressure at the surface of the earth. Please show us how the manual solution got the pressure at 7.6 km.

Chet
 
This is from the solution manual:

The gauge pressure at a depth of 20 m in seawater is
p1swgd = 2.00 x 105 Pa
On the other hand, the gauge pressure at an altitude of 7.6 km is
p2airgh=6.48 x 104 Pa
Therefore, the change in pressure is
Δp = p1 - p2 = 1.4 x 105 Pa
 
dmk90 said:
This is from the solution manual:

The gauge pressure at a depth of 20 m in seawater is
p1swgd = 2.00 x 105 Pa
On the other hand, the gauge pressure at an altitude of 7.6 km is
p2airgh=6.48 x 104 Pa
Therefore, the change in pressure is
Δp = p1 - p2 = 1.4 x 105 Pa
The result for 7.6 km from the solution manual is incorrect. They have the sign wrong. It should be p2= - ρairgh= - 6.48 x 104 Pa. The absolute pressure at 7.6 should be 1. x 105 - 6.48 x 104 Pa. This is where the atmospheric pressure at the surface comes in.

Of course, this error makes the final answer incorrect also.

Chet
 
Isn't 105 only applies to things at roughly sea level? Wouldn't something at 7.6 km up not be subjected to this pressure?
 
dmk90 said:
Isn't 105 only applies to things at roughly sea level? Wouldn't something at 7.6 km up not be subjected to this pressure?
Sure. It''s less. That's what I calculated.

Chet
 

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