2 ms·
The fuselage isn’t being stressed in a wing load test. There is zero way the fuselage could stand up to the level of force being applied to the wings.
by stouset 2y ago
The fuselage isn’t being stressed in a wing load test. There is zero way the fuselage could stand up to the level of force being applied to the wings.
- hinkley 2y agoI would submit to you that it’s impossible to load the wings at 150% of max load without transferring any of that force into the fuselage. Look at any finite element analysis of complex shapes. The force spreads out from areas of max tension or compression, and goes around corners.