Drag coefficient

team47b

fd =1/2 pv2 cd A

Or possibly simply... 0.47

team47b

I can't imagine what I must of posted on that other forum :oops:

AlexMac1973

team47b wrote:

fd =1/2 pv2 cd A

Or possibly simply... 0.47

Is this equation still relevant in respect to how to solve a problem like a ladyboy? And does that mean given there preference they also are drag coefficient?

GiantMike

team47b wrote:

fd =1/2 pv2 cd A

Or possibly simply... 0.47

You need to check your working. What are you using for fd, p and A?

Is your cd dimensionless?

team47b

It is spherical so it is 0.47

pinno

"Co-efficient of lift x 1/2 air density x the velocity squared x the plan area of the wing. Coefficient= angle of attack and shape of the aerofoil. Drag is CD1/2pV2S."

I cannot think why T47b wants to dress up as a woman and strap himself to a wing of some description, whilst singing 'Life is a Cabaret'.

team47b

pinarello001 wrote:

"Co-efficient of lift x 1/2 air density x the velocity squared x the plan area of the wing. Coefficient= angle of attack and shape of the aerofoil. Drag is CD1/2pV2S."

I cannot think why T47b wants to dress up as a woman and strap himself to a wing of some description, whilst singing 'Life is a Cabaret'.

Slow week