---------------------------------------------------------- TeamGrumman-List Digest Archive --- Total Messages Posted Sun 09/12/04: 2 ---------------------------------------------------------- Today's Message Index: ---------------------- 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 _____________________________________ Time: 10:36:18 PM PST US From: TeamGrumman@AOL.COM Subject: Re: TeamGrumman-List: 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 _____________________________________ Time: 10:39:12 PM PST US From: TeamGrumman@AOL.COM Subject: Re: TeamGrumman-List: 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.'