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how to calculate and apply the pressure load in patran

how to calculate and apply the pressure load in patran

how to calculate and apply the pressure load in patran

(OP)
actually i want to simulate a wing which is in 1g flight condition . now i want to apply pressure load which is equal to 1g flight condition . can u tell me how to carry this . i gone through some patran tutorials , i didnt get any proper info. is there any standard formula which relates pressure and flight condition .

RE: how to calculate and apply the pressure load in patran

research "schrenk" distribution. this describes the spanwise load distribution on a wing

Quando Omni Flunkus Moritati

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