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"Robert M. Gary" wrote:
at first Boeing didn't believe it really happened until they sent their engineers out. They explaination is that the body itself generates so much lift it could still fly. If this account is true, then what does this say about the engineers of this aircraft? Isn't the lift generated by the body itself taken into account by these engineers? -- Peter |
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![]() "Peter R." wrote in message ... "Robert M. Gary" wrote: at first Boeing didn't believe it really happened until they sent their engineers out. They explaination is that the body itself generates so much lift it could still fly. If this account is true, then what does this say about the engineers of this aircraft? Isn't the lift generated by the body itself taken into account by these engineers? -- Peter Yeah, but... At first glance, the engineers probably looked at first order issues - can the airplane fly straight and level with most of one wing missing? I'm sure they had enough data in their files to say... At a certain speed, the good wing generates X pounds of lift and a rolling moment of Y pound feet. The remaining aileron can generate a rolling moment of Z pound feet to counter the rolling moment from the wing. The answer was probably that Y Z, so the aircraft would be uncontrollable. As Dudley pointed out, there was probably a significant yaw induced due to the asymmetric airframe. This would have reduced lift on the existing wing, reduced the rolling moment, and allowed the wide fuselage to generate enough lift at 250 knots to bring the airplane home. It is very doubtful that the engineers had data for that flight condition at hand to override the initial analysis based on the data they did have... KB |
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