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Re: Absolutely Nothing

By: Cactus Flower in ALEA | Recommend this post (0)
Thu, 19 Jun 14 6:05 PM | 33 view(s)
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Msg. 15659 of 54959
(This msg. is a reply to 15658 by faul)

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hi doma,

i think you don't understand mach numbers!

mach numbers are dimensionless. the shock wave is the same at different altitudes so long as you fly at the same mach number.

this is why the manufacturers define the air frame's limits using a mach number.

it may not sound like common sense. but it is what it is.

once you know this, first you understand the plane was capable of flying at the recorded velocity, then that there was no conspiracy, and then that the universe is random rather than controlled!!

that is, unless the desire to believe in conspiracies is the fixed point to which all your theories are tethered.


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The above is a reply to the following message:
Re: Absolutely Nothing
By: faul
in ALEA
Thu, 19 Jun 14 4:35 PM
Msg. 15658 of 54959

Hi Alea.....

D = ½�V2SCD

Air Density at Sea level.......23.77p
Air Density at 35,000 ft........7.38p

So both you & this expert Believe that air density
& velocity have no effect on drag & that drag has
no effect on an aircraft's airframe or engine's
maximum output thrust.

Throw physics & common sense out the window &
engage your belief system!


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