Experimental VG's for the exit air flow...
Ok here's the project?
Today I build four vortex generators out of 1 1/2" x 1 1/2" x 1/16" alum stock, I made them 3" long with the square edges.
I placed two at a 40deg angle to one another 3" apart in front of the nose wheel fairing. I also placed two at a 40deg angle 6" apart on the lower cowl just in front of the exhaust pipes.
I'm trying to lower the CHT's by cleaning up the exit air.
Before VG's:
MAX POWER CLIMB
80KTS
FULL POWER
To 3800 MSL from 580 MSL
max CHT 447
CRUSE test
2500 rpm
OT 71 deg
max CHT 348 (all CHT's within 7 deg)
3800' MSL
After VG's:
MAX POWER CLIMB
80KTS
FULL POWER
To 3800 MSL from 580 MSL
max CHT 441
CRUSE test
2500 rpm
OT 71 deg
max CHT 338 (all CHT's within 7 deg)
3800' MSL
The question is....
Is it worth the trouble to continue this approach for 10 degs?
or
I'm I just barking up the wrong tree?
Sorry no pictures ... I didn't even know if this was going to do anything at all.
__________________
(This post by: Christopher Checca EAA Lifetime Member #799388)
Allen Checca (father)
Christopher Checca (son)
RV-6A - N468AC
ENGINE: Lycoming 180 HP O-360-A1A
PROPELLER: Senisentch 72FM859-1-85
WEIGHT: Empty Aircraft 1152 lbs
BASED: KC09 - Morris, IL.
Flying since June 6, 2005
N468AC Web Site
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