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Assuming 50% efficiency (I think this is the wrong term; it should be 'effectiveness'; but it's the one they use, and simply means the temperature drop across the intercooler divided by the temperature difference between the charge air and the ambient air), that would mean 22 degrees less temperature reduction if cowl air were used. Goaded by Peter Lert, I broke the solder joints to the dead battery in the Lowrance and extracted it, a 3v Renata CR2450N valued at .
Following his advice, I crammed a new battery in with padding to press the contacts against it, and voila, it remembers! My design process has always involved obsessively thinking about the object to be designed. My recollection of the details of the engine compartment is not so complete or exact that I can mentally map every attachment and duct path, but I have dozens of photographs of it to help me. The intercooler must be able to be built piecemeal, without having to ground the airplane for long at any stage.
I remember, during the construction of Melmoth 1, intensely visualizing the retraction linkage for the main landing gear while meditating at the Cimarron Zen Center of Rinzai-ji. It must be easy to remove, with as few attachment points as possible, and have short, direct flow paths.
It must require moving or damaging as few existing items as possible.
On the other hand, it seems to have forgotten its airport and navaid data, and now offers only user waypoints in response to the "Goto" command.
It's evident, anyway, that there's a good deal of heat to be gotten rid of.I'm not sure what the politics of splitting the inner channel of a NACA scoop are, but I'll find out.The most difficult part of the whole project, I think, will be making the induction-air tanks, which have to withstand both heat and pressure.(I am reluctant to attach such a large, relatively massive object to the engine.) I have not yet found out how much cooling air the intercooler requires.A turbonormalized Bonanza has a ram air intake about 3 or 3.5 inches in diameter, but unless the velocity ratio in the duct happens to be 1.0, that tells me little about the actual mass flow.