PPRuNe Forums - View Single Post - Relation between IAS and Mach number
View Single Post
Old 5th Jun 2006, 03:30
  #33 (permalink)  
rhovsquared
 
Join Date: Jun 2005
Location: NY
Posts: 278
Likes: 0
Received 0 Likes on 0 Posts
ohh I'm glad this is back

RivetGun Are you flying in Vacuo????
you can't take moles out of it the adiabatic gas laws don't allow that: Cp-Cv=nR, Y=Cp/Cp+nR


and I didn't say T dependent I said Rewrite as a function of T

ex: dw = -PdV and du = CvdT and dU = dw+dq adiabatically = du = dw

so I can say Cvdt=-Pdv; REWRITING P in terms of T

Cv dT/ T = -nR dV/V since Cv is a constant I can integrate then i have

<Tf/ (dT/T) / Ti> = -nR <Vf / (dV/V) /Vi > = lnTf/Ti = -nRln (Vf/Vi)

using a ln X =lnX^a

and gas laws,

I have Ti/Tf = (Vf/V1)^y

lastly, Pi Vi^y = Pf Vf^y.

applying this judiciously with the equation fo dynamic pressure you can derive the equations (corrected for adiabatic compressibility) provided by Old Smokey
with about four pages of algebra...I' m not doing it

p.s. please let me know if I made an error if anyone finds one


edited: to correct a error Cp DIFFERS from Cv by nR NOT Cp+Cv=nR

I was very wrong there!!!

Last edited by rhovsquared; 8th Jun 2006 at 20:11.
rhovsquared is offline