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  • Congratulations waross on being selected by the Eng-Tips community for having the most helpful posts in the forums last week. Way to Go!

WKTaylor's latest activity

  • WKTaylor
    WKTaylor replied to the thread BOOM lives up to its name.
    Back to the 1960s... Boeing 2707... Problem #1: Boeing had NO experience with supersonic flight...
  • WKTaylor
    WKTaylor replied to the thread Tolerance of Upset Rivet Head.
    Also... MIL-STD-403 PREPARATION FOR AND INSTALLATION OF RIVETS AND SCREWS, ROCKET, MISSILE, AND AIRFRAMS STRUCTURES MIL-STD-40007...
  • WKTaylor
    WKTaylor replied to the thread Threaded Rod Design.
    Push-pull rods... and could-be adjustable strut-rods... to take-a-look-at.... NAS91-thru-NAS119 NAS354-thru-NAS373 NAS37 Rod-End...
  • WKTaylor
    WKTaylor replied to the thread Threaded Rod Design.
    Related... my company specifies push-pull rods or struts... with one end fixed, other end adjustable... have very special design...
  • WKTaylor
    WKTaylor replied to the thread Tolerance of Upset Rivet Head.
    How I would have written this table... Tolerance of upset [bucked/squeezed] rivet tail, D= rivet shank diameter Dia Max= 1.66 x D...
  • WKTaylor
    WKTaylor replied to the thread tail moment imbalance.
    FAA AC 23-9 - [Large AC] Evaluation of Flight Loads on Small Airplanes with T, V, +, or Y Empennage Configurations Design Process...
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