Tantalum
Final Approach
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San_Diego_Pilot
Last message.. then I'm done spamming this thread for a bit
Give it a bigger engine or dive go fast sure, if you can generate the airspeed needed to maintain lift.. but if I load a PA-28 up to 500 lbs over gross it's either (A) not going to take off or (B) not climb well. The wing's structure (so to speak) will have no idea that it's trying to carry more when going 75 knots. It's going to feel that same sub V(a) lifting force whether it's trying to lift 2,400 lbs or 240,000 lbs. It can only generate X amount of lift.
Either that or I'm thinking about this all wrong
Right but these structural exercises are assuming the wing is capable of lifting that. To me it's like arguing that a hot air balloon's envelope will fail if you put too many people in the basket. As is with the balloon, it just won't rise, or climb as well. The wing, assuming all else is equal, can only generate so much lift, especially if staying under V(a)on't forget that 2.8g has to multiplied by the weight to get the total force acting on the structure. 2.8g is the limit when at max weight
Give it a bigger engine or dive go fast sure, if you can generate the airspeed needed to maintain lift.. but if I load a PA-28 up to 500 lbs over gross it's either (A) not going to take off or (B) not climb well. The wing's structure (so to speak) will have no idea that it's trying to carry more when going 75 knots. It's going to feel that same sub V(a) lifting force whether it's trying to lift 2,400 lbs or 240,000 lbs. It can only generate X amount of lift.
Either that or I'm thinking about this all wrong