By A. S. Taylor, D. J. Eckford (Eds.)
Read or Download Aircraft Loading Action Problems (Proceedings of a Symposium held at Farnborough on 28th October, 1966) PDF
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Extra resources for Aircraft Loading Action Problems (Proceedings of a Symposium held at Farnborough on 28th October, 1966)
Dealing with the time when the tailplane to the time of maximum tailhowever,is loaded not only loads on the tailplane, is a maximum the inertia conversely, when the inertia factors are a maximum the its peak. ) In this case it is a relatively the worst loads but this type of problem becomes timeoases where everything is varying with time and a search interval has to be done for practically every item of This subject gust loads. is discussed in more detail The checked manoeuvre cases have to be investigated down en route and in the flaps-down landing configurations.
Mr. F'insker said that one area in which he had become involved in Loading Actions was that of inertia cross-coupling. There,a large amount of the trouble stemmed from allowing the pilot to use the controls in a way which was of no utility and very often it was possible to eliminate the problems altogether by putting stops on the control surfaces. He wondered whether many time-honoured concepts, even n, and so on, could not be revised very sharply if scme means could be found to restrict the manceuvres to those that were really necessary.
Mr. Hufton emphaslsed that a lot of knowledge had already been galned but that even more was demanded by modern levels of sophistication. g. by automatic would have additional implications. Mr. M. , controls, Board of Trade though referred I . i he knew this to Mr. Goldberg's query about vertxal velocities of descent and whether the attitude of the aeroplane, or the lift on the aeroplane, was being considered. He said that flight measurements of touchdown parameters were being made at Heathrow and that these could have a bearing on the subject.