Today's Message Index:
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1. 10:36 PM - Re: AA-1 O-320 upgrade Air Box/Intake Geometry (TeamGrumman@AOL.COM)
2. 10:39 PM - Re: Engine Cowling Alignment Question for AA5B (TeamGrumman@AOL.COM)
Message 1
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| Subject: | Re: AA-1 O-320 upgrade Air Box/Intake Geometry |
--> TeamGrumman-List message posted by: TeamGrumman@aol.com
In a message dated 9/11/04 12:32:45 AM, steven.jackson14@adelphia.net writes:
> Is there a resource online or a reference book that has the
> formulas/equations for figuring the different inlet sizes and explaining the
whole concept
> of pressure recovery?
>
> Steve
>
There is probably a book out there somewhere.
When I was doing flight test at Edwards, and got bored, I worked out the
equations, putting it on scratch paper on my cubicle wall. I eventually entered
it into a database. I run it on Filemaker. I also worked out the equations
for sequential port fuel injection ... but that is a different story.
Message 2
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| Subject: | Re: Engine Cowling Alignment Question for AA5B |
--> TeamGrumman-List message posted by: TeamGrumman@aol.com
In a message dated 9/10/04 1:21:02 PM, NewmanRic@AOL.COM writes:
> After the newly overhauled engine was installed the prop spinner is about
> .3 inches too high and .3 to .4 inches to the right of center when viewed=20from
> behind the prop.=A0
>
Try changing the spacers between the block and the engine mount bushing.
The alignment is 'shim to fit.'
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