Mailing List flyrotary@lancaironline.net Message #27114
From: Bob White <bob@bob-white.com>
Subject: Re: [FlyRotary] Re: specific heat of air
Date: Fri, 21 Oct 2005 19:25:36 -0600
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Hi Ed,

Al's number was .02 BTU/cu-ft. - F and your number is 0.241 BTU/lb - F.
Per the web site you mentioned, density is given as 0.08018 lb/cu-ft.
So if I'm doing the conversion in the right direction:
0.241 X 0.08= 0.019 which is about 0.02.

Are both numbers correct?

Bob W.



On Fri, 21 Oct 2005 20:46:02 -0400
"Ed Anderson" <eanderson@carolina.rr.com> wrote:

Al, I went back to some of my spreadsheets and I have for constant pressure (Cp) as 0.25 BTU/Lbm/F

Here is web site which gives it as 0.241 BTU/LBM/F at 32F Sea Level

http://www.uigi.com/physical_prop_e.html

So looks like you have the decimal off a bit.

Sorry, it took me so long, been out at the aircraft all day putting on the new right gear leg, and brakes, etc.

Ed A




  ----- Original Message -----   From: Al Gietzen   To: Rotary motors in aircraft   Sent: Friday, October 21, 2005 2:59 PM
  Subject: [FlyRotary] specific heat of air


  Ed, or Bill, or somebody; help me out here.  I was reviewing my calcs for air flow requirements, and find I used 0.02 Btu/cu. ft -F for the specific heat of air.  I don't know where that came from, and can only find it in joules/Kg - K.  By the time I do all the conversions to British units and mass to volume I now get quite a different number.



  What is a good number for air at about 1 atmosphere and, say 90F; in Btu per cu ft per degree F?



  Thanks,



  Al



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