| Subject: Cooling drag fallacies |
| From: Paul |
| Date: 10/7/1999, 8:44 PM |
| To: zz |
X-Mozilla-Keys: Al Gietzen wrote:
Fred: 1. How about a similar look at the pusher prop case as in a Velocity or EZ? Inlets below or above the wing or fuselage near the leading edge of the rear engine cowling. 2. I Assume that the outlet as small as possible means at least the square of the oulet to inlet temp ratio times the inlet area? Thanks, Al Gietzen
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