Robert, That patch of glass you showed that’s “not wetted out enough with dry spots” looks like the original inside layer of the factory fuselage shells. The factory shells were (apparently) not made

Paul, You’re thinking of the Q2 wing. The Q1 wing shear web ends at BL52. See plans page 9-6: https://davidjgall.com/Q/Quickie/Quickie%20Plans/Quickie%20plans%20section%2009.pdf. David J. Gall

Cody, I agree with the syringe/micro repair but I disagree with the procedure. Don’t just shoot micro down into the delaminated area. First, use a quarter to do the tap test and map out the delaminate

That must be a node where the bending energy was focused when the prop experienced resonance.

Heeeyyyyy! I resemble that remark!! 😅

Michael makes an excellent point about comparisons between props. There is much, much more to props than just the diameter and pitch.

FWIW, I concur with Jay’s analysis and explanation here. David J. Gall

Robert, There is a minimum length requirement otherwise you’ll end up with warped exhaust valves from cyclic cooling. For estimating drag, a rule of thumb is to imagine each pipe extended 12-15 inches

Point of reference: A cold-call to Ly-Con about F1 horsepower several years ago resulted in a 1-1/2 hour discussion with their dyno technician. He told me that the O-200s on F1 racers produce about 16

“Most all” F1 racers are also at the back of the pack. Just sayin’.

See if what you need is in this .ZIP file. https://davidjgall.com/Q/LS(1)%20canard/LS(1)%20canard%20plans.zip

😆

Oh, my!

Bill, That’s unfortunate. I’m betting that person has impeccable credentials, too. There will always be those few and their ardent followers. Hard as one might try, one cannot force right-thinking. I

What do you need help with, Bill? First you want us to go to another group and immerse ourselves in their imbroglio and now you want to slap down someone you think is somehow lesser than you? You migh

Nooooooo! No no no no no no nooooooo! Those Keyboard warriors put more bullshit through my head in ten minutes of reading their collective ignorance than I’ve seen in FORTY YEARS of reading and studyi

Mike, did you notify the FAA since that’s a certified part? They might be interested.

EZ-87 is still available and is the slow hardener having a 5-hour pot life. EZ-84 is no longer available, but that was a low viscosity formulation for RTM (infusion). Last I checked, MGS was not avail

Yeah, that’s Mike alright. He’s walking without a limp and he bent down to get his hat out of the wreckage so it appears that he’s all good. Mike, you did good picking a landing site. It looks like yo

Michael, Fun history tangent noted. Regarding your reported airfoil discrepancies, is it possible that you are inadvertently comparing two different airfoils, the LS(1)-0417 from the NASA TM against t