Joe,
The cooling air exit needs to be pointed aft like a jet engine exhaust.
Blast to the rear, not down.
Sorry if my semantics have created any confusion.
Sid Wood
Tri-gear KR-2 N6242
Mechanicsville, MD, USA
--
From: "Joe. E. Wallace"
Enjoyed your comments on air
Here is my experimentation into this very issue.
http://kr2spacemodulator.blogspot.com.au/search/label/KR2S-02%20Fuselage
Basically a thrust augmentation/extraction system.
As I am not flying yet I can't give you any results.
Paul.
Brisbane, Australia
-Original Message-
From: Sid Wood vi
Sid Wood
Enjoyed your comments on air movement and if I understand your comment
< abetter scheme is to make a rear facing ramp to get the air flowing
smoothly toward the exit with the exit cut off square with the slip
stream.>>>
would mean that the cut off of the discharge is 90 d
Pete,
The idea for the larger opening size is to accommodate the increased air
volume due to engine heating. However, the exit methodology is particularly
critical to the overall efficiency for getting the cooling air overboard and
back into the airstream. Simply cutting a big hole in the bottom
Netters
I working on the lower half of my cowling and need to know the multiplier to
size the exit area. I vaguely remember that the exit area should be approx. 1.5
times the total size of the inlet area. Need to qualify that memory. I have
Tony Bingelis' "Firewal Forward" book, but can't find
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