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Search: Posts Made By: megan
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Forum: Questions
9th Nov 2020, 04:25
Replies: 14
Views: 3,970
Posted By megan

You're explanation is lacking in why the CL would...

You're explanation is lacking in why the CL would be different. If B has a different CL to A, but wing area and velocity are the same, that would mean that the one with the higher CL would be...
Forum: Questions
7th Nov 2020, 22:54
Replies: 14
Views: 3,970
Posted By megan

Beg to differ. Given the attributes you describe,...

Beg to differ. Given the attributes you describe, same wing area different airfoil, the Cl will be the same, as the formula shows.

L=0.5*A*ρ*CL*V^2

where:

L = Lift force
A = Surface Area
V...
Forum: Questions
26th Oct 2020, 04:39
Replies: 14
Views: 3,970
Posted By megan

There is no "additional lift". Best think of a...

There is no "additional lift". Best think of a propeller, it's just an airfoil that gets its airspeed by rotating, the pressure difference between the forward and rear faces causes the airflow to...
Forum: Questions
16th Oct 2020, 20:33
Replies: 14
Views: 3,970
Posted By megan

The coefficient of lift, which is a dimensionless...

The coefficient of lift, which is a dimensionless number, expresses the ratio of the lift force to the force produced by the dynamic pressure times the area.

Cl = L / (q * A)

Cl = coefficient...
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