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Female Submissive, 44, england
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Female Submissive, 44, Houston, Texas
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Female Submissive, 35
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About Bubble78
Lift coefficient
Main article: http://en.wikipedia.org/wiki/Lift_coefficient
If the lift coefficient for a wing at a specified angle of attack is known (or estimated using a method such as http://en.wikipedia.org/wiki/Thin-airfoil_theory), then the lift produced for specific flow conditions can be determined using the following equation:
where
- L is lift force,
- ρ is air http://en.wikipedia.org/wiki/Density
- v is http://en.wikipedia.org/wiki/True_airspeed,
- A is http://en.wikipedia.org/wiki/Planform area, and
- CL is the lift coefficient at the desired angle of attack, http://en.wikipedia.org/wiki/Mach_number, and http://en.wikipedia.org/wiki/Reynolds_number
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Male Dominant, 56, Omaha, Nebraska
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Male Submissive, 45, New York City, New York
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Male Submissive, 46, Carlinville, Illinois
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Male Submissive, 35, oblong, Illinois
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Male Dominant, bumfuk, Minnesota
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