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Re: Re-jet carb for high altitude?
Posted to Technical Theory Forum on 6/29/2009 4 Replies

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P1-P2 = Rho*(V2^2-V1^2)/2

In the case we are discussing (constant rpm, or flow velocity), V2 and V1 don't change - so the term in brackets is a constant - and can be replaced with a lumped constant... Login to read more.

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