By A. S. Taylor, D. J. Eckford (Eds.)
Read Online 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)
As a result, the peak loads in the two dxeotlons may not oolncide. This alleviates the maximum loads. Also for most components either fv is much larger than fs, or vice versa, and the maximum stress XI, therefore, not much greater than that in the simple case. , when design work 1959, that the axoraft would be deslgned to meet The gust clock' gusts oomlng from any dxeotion. normal values of 66 ft/seo at VB, 50 ft/seo at VC on the Trident started In the case of 'round-thevelooitles were to be the and 25 ft/seo at VD.
I. over the whole aircraft together with the correspitching moment coefficient and aerodynamic centre. inverted since it is usually the overall coeffrom wind tunnel tests and the distributions agree with the overall values. As mentioned above, the introduction of aircraft with flexible swept wings has further complicated the calculation of the design loads on the wing tip deflects wings in the symmetric manoeuvre oases. The Trident about 60 inches under limit load. Since the wing is swept at 30' and the bending takes place along the swept flexural axis it follows that there is an 'in line of flight' change of wing incidence equal to the bending slope times the sine of the angle of sweepback.
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. 2 manoeuvre and design Aileron cases Lateral control cases produce design loads in a later also section in the flaps- in parts of the almost the whole tailplane.
Aircraft Loading Action Problems (Proceedings of a Symposium held at Farnborough on 28th October, 1966) by A. S. Taylor, D. J. Eckford (Eds.)