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- W2054698978 abstract "A method of analysis with which to determine both the static elastic deformation and associated change of aerodynamic characteristics of a flight vehicle subject to aerodynamic and inertia loading is presented. The general approach to the static aeroelastic analysis is to present the integral equations representing the aerodynamic loading and the structural deformations to a system of related influence functions suitable for numerical evaluation by digital computers. Thus, by representing the aerodynamic and structural characteristics of a configuration by a system of equivalent lumped parameters, sets of influence coefficients relating the elastic deformations to the aerodynamic and inertia loading are developed and then cast into a system of matrix equations for solution. This analysis is applicable to a lifting body experiencing a given flight environment. Specifically, the analysis evaluates the aerodynamic characteristics and camber distribution of an elastic body influenced by aerodynamic and inertia loads." @default.
- W2054698978 created "2016-06-24" @default.
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- W2054698978 date "1965-12-01" @default.
- W2054698978 modified "2023-09-27" @default.
- W2054698978 title "General static aeroelastic analysis for a body of revolution." @default.
- W2054698978 cites W1518201591 @default.
- W2054698978 doi "https://doi.org/10.2514/3.3354" @default.
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