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  • Users: macoovacany
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  1. macoovacany

    Paint Approval Considerations

    What type of engineering considerations (corrosion prevention, electrical conductivity,...(?) ) needs to be made when approving particular painting materials, e.g. paint stripper, filler, primer, topcoat, etc. 1) Story going around of a private owner who used automotive wax for buffing his a/c...
  2. macoovacany

    Twin Engine Propeller Arc

    How come the propeller arc is behind the pilot in high wing twins (MU-2, Partnavia, Aerocommander) and in front of the pilot in low wing twins (Cessnas and Pipers). Cheers, Timbo
  3. macoovacany

    Rolled Threads and Fatigue

    Hello all, I have a specially made bolt/stud that requires remanufacture. A materials analysis of the bolt indicates that the threads have been rolled. A quick search on the internet indicates that rolled threads offer 30%-70% improvement in fatigue stress or a ten-fold increase in service...
  4. macoovacany

    Stress Determination by Crack Inspection

    Hello all, Consider a crack in the middle of large sheet of metal, about the same dimensions as, say, the sidewalls of the engine bay mount for the Cessna 210. The crack was probably initiated by a tool scratch, falling screw driver, whatever. There is now a crack that runs at approximately...
  5. macoovacany

    Cad-plate fatigue life

    As standard practise, we specify the cad-plate of all steel parts we design to QQ-P-416F. However, it has come to our attention that this may dramatically reduce the fatigue life. On page 287 of "Mechanical Engineering Design" by Shigley and Mischke it states "Metallic coatings...
  6. macoovacany

    Curly ATA question

    This question is a bit off engineering, but maybe interesting none the less. The Beechcraft Baron has an "aft cabin door ajar" warning light. Where do you think that this should appear in the ATA code? a) 52 : Doors b) 33 : Lighting c) 31 : Indicating and recording systems Have fun...
  7. macoovacany

    Body of Revolution Pressure Distribution

    Hello, Does anyone know how to derive the pressure distribution of a body of revolution given the geometric section properties. Kind of have the feeling that it is equivalent to the 2-D flow pressure distribution, if the thicknesses were sqrt'ed. Timbo
  8. macoovacany

    Rivet Patterns

    Which rivet pattern is stronger? (Ignore number of rivets.) + + + + + + + + + + + + or... X X X X X X X X X X X X X X
  9. macoovacany

    Vee-tail flutter

    Hi. Anyone know any reports or had any experience with Vee-tail flutter characteristics. I'd imagine that it's be worse since the ruddervators can not have a torsionally stiff connection, which has been a requirement for elevators since the 1920's. Timbo
  10. macoovacany

    Turbine Engine Exhaust

    Howdy all, Well since diffusers didn't grab your attentin, how about this? How should you design the exhaust stack for a turboprop to maximise cruise efficiency? Specifically PT6. Manufacturers installation manual appears somewhat inadequate. The results from their CCD program gives a...
  11. macoovacany

    Intake Diffusers

    Hello, I am looking for engineering information on inlet diffuser design. Specifically, angle versus length data for stable flow and maximum pressure rise and minimum drag and energy losses. Regards, Timbo

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