pontiacjack
Electrical
- Apr 16, 2007
- 194
Hi. I'm new to this particular forum, and hoping for some guidance on a project that's in the early planning (dreaming?) stage.
I bought a proven "lakes" race car (belly-tank lakester) and will be building a blown-alky four cylinder hemi engine for it (182 c.i. for class-F, where the SCTA record is 262 MPH). In order to get anywhere near the record, I'll need about four HP/c.i. (~720 HP). Engine simulations (using actual measured port flow of my head) reveal the need for 33 PSIG manifold pressure (@ 14:1 static c.r.). This is do-able, but I'm concerned about rotational speed of the blower- an 8-71 would need to be driven 47% over crank, which would put the blower rotors at darn near 15K RPM at peak-power speed of the engine (~10K RPM)!
"Conventional wisdom" won't help me answer this question, since I've already run a BDS 6-71 much faster (and longer) than it "should" have survived- two full competition seasons at rotor speeds just shy of 10,000 RPM. [However, it's a small-bore 6-71]
I see two areas of concern: 1) rotor integrity (explosion?)
and 2) behavior of the fluid flow at such elevated rotor tip speeds (turbulent and inefficient?).
Any and all comments are welcome...
I bought a proven "lakes" race car (belly-tank lakester) and will be building a blown-alky four cylinder hemi engine for it (182 c.i. for class-F, where the SCTA record is 262 MPH). In order to get anywhere near the record, I'll need about four HP/c.i. (~720 HP). Engine simulations (using actual measured port flow of my head) reveal the need for 33 PSIG manifold pressure (@ 14:1 static c.r.). This is do-able, but I'm concerned about rotational speed of the blower- an 8-71 would need to be driven 47% over crank, which would put the blower rotors at darn near 15K RPM at peak-power speed of the engine (~10K RPM)!
"Conventional wisdom" won't help me answer this question, since I've already run a BDS 6-71 much faster (and longer) than it "should" have survived- two full competition seasons at rotor speeds just shy of 10,000 RPM. [However, it's a small-bore 6-71]
I see two areas of concern: 1) rotor integrity (explosion?)
and 2) behavior of the fluid flow at such elevated rotor tip speeds (turbulent and inefficient?).
Any and all comments are welcome...