ANALYTIC SENSITIVITIES IN COMPOSITE WING-SHAPE YNTHESIS PART TWO: PANEL FLUTTER CONSTRAINTS
نویسندگان
چکیده
منابع مشابه
analysing panel flutter in supersonic flow by hopf bifurcation
this paper is devoted to study of a partial differential equation governing panel motion in supersonic flow. this pde can be transformed to an ode by means of a galerkin method. here by using a criterion which is closely related to the routh-hurwitz criterion, we investigate the mentioned transformed ode from hopf bifurcation point of view. in fact we obtain a region for existence of simple hop...
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ژورنال
عنوان ژورنال: International Conference on Aerospace Sciences and Aviation Technology
سال: 1999
ISSN: 2636-364X
DOI: 10.21608/asat.1999.24893