Terminal Velocity Calculation: Air Density & Drag Coefficent

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SUMMARY

The terminal velocity of a falling object can be calculated using the equation provided on Wikipedia. For a 57 kg individual at an altitude of 1000 meters, the drag coefficient and air density are critical parameters. Typical values for the drag coefficient for a human body range from 0.7 to 1.0, while the air density at 1000 meters is approximately 1.112 kg/m³. These values are essential for accurate terminal velocity calculations.

PREREQUISITES
  • Understanding of the terminal velocity equation
  • Knowledge of drag coefficient values
  • Familiarity with air density variations with altitude
  • Basic physics concepts related to forces and motion
NEXT STEPS
  • Research the effects of altitude on air density using the International Standard Atmosphere model
  • Explore the relationship between drag coefficient and object shape
  • Learn how to calculate terminal velocity for different weights and shapes
  • Investigate the impact of wind resistance on falling objects
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Physics students, engineers, and anyone interested in understanding the dynamics of falling objects and terminal velocity calculations.

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Not a homework question as such, but I thought this was the best place to put it.

I'm trying to work out the terminal velocity of a falling object, say myself (57kg) at 1000m, I have the equation from http://en.wikipedia.org/wiki/Terminal_velocity but have no idea what the drag coefficient is or the density of air at that altitude. Does anyone know what these values are?
 
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Here are some typical values

http://www.ac.wwu.edu/~vawter/PhysicsNet/Topics/Dynamics/Forces/DragCoeficientValues.html
 
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