Pietenpol-List: negative G loading for Piet wing
Posted: Wed Jun 15, 2011 10:45 pm
Original Posted By: Michael Groah
Mark asked->Do you know what the negative-G stress loading is on a pietI'm not aeronautical engineer and I didn't sleep in a Holiday Innlast night, but my napkin sketches and calcs indicate that negativeG loading is a weak point of the Piet structure. I may also bevery mistaken when I write this, but I believe one of the few knownstructural failures of a Piet was when one fell out of a loop or attempted a negative-G maneuver and the struts collapsed.Normal category loading for certified aircraft is +3.8 and -1.52Gand the Piet is certainly no better rated than that, IMHO.Oscar ZunigaAir Camper NX41CCMedford, OR ________________________________________________________________________________
Mark asked->Do you know what the negative-G stress loading is on a pietI'm not aeronautical engineer and I didn't sleep in a Holiday Innlast night, but my napkin sketches and calcs indicate that negativeG loading is a weak point of the Piet structure. I may also bevery mistaken when I write this, but I believe one of the few knownstructural failures of a Piet was when one fell out of a loop or attempted a negative-G maneuver and the struts collapsed.Normal category loading for certified aircraft is +3.8 and -1.52Gand the Piet is certainly no better rated than that, IMHO.Oscar ZunigaAir Camper NX41CCMedford, OR ________________________________________________________________________________