VO wrote:

We all looking for better way to make more efficient cooling.
      NACA (NASA) submerged inlets the best solution!
I believe it is important to make correct profile for NACA scoops. So,
Based on NACA (NASA) research of 1945, 1948, 1951 and modern
research, I put together EXCEL worksheet which help to calculate
NACA submerged inlets. It is easy to use, and it is free for download.
Go to my web page at:
   http://www.n1ut.velocity-air.com
There are also links on a few articles on theory of NACA submerged inlets.
If you have any questions, please do not hesitate to ask.
Vlad

N1UT - Velocity Elite, RG, Mazda 20B rotary, NA - in progress
http://www.N1UT.velocity-air.com

 
The Aircraft Rotary Engine Newsletter.              Powered by Linux.

http://home.earthlink.net/~rotaryeng/            http://www.linux.org