in the Hessian is well conditioned while the aerodynamics part is ill conditioned. It should be emphasized that in this The symbol of the Hessian for a static aeroelastic optimization model problem is analyzed for the optimization of a plate's shape study the shape of the plate is allowed to change
Efficient optimization of integrated aerodynamic–structural design
✍ Scribed by R. T. Haftka; B. Grossman; W. M. Eppard; P. J. Kao; D. M. Polen
- Publisher
- John Wiley and Sons
- Year
- 1989
- Tongue
- English
- Weight
- 874 KB
- Volume
- 28
- Category
- Article
- ISSN
- 0029-5981
No coin nor oath required. For personal study only.
✦ Synopsis
The introduction of composite materials is having a profound effect on the design process. Because these materials permit the designer to tailor material properties to improve structural, aerodynamic and acoustic performance, they require a more integrated multidisciplinary design process. Because of the complexity of the design process numerical optimization methods are required.
The present paper is focused on a major difficulty associated with the multidisciplinary design optimization process its enormous computational cost. We consider two approaches for reducing this computational burden: (i) development of efficient methods for cross-sensitivity calculation using perturbation methods; and (ii) the use of approximate numerical optimization procedures. Our efforts are concentratcd upon combined aerodynamic-structural optimization. Results are presented for the integrated design of a sailplane wing. The impact of our computational procedures on the computational costs of integrated designs is discussed.
📜 SIMILAR VOLUMES
This paper describes a hovering rotor blade design through the suitable combination of flow analysis and optimization technique. It includes a parametric study concerned with the influence of design variables and different design conditions such as objective functions and constraints on the rotor pe
The one-and two-dimensional inviscid Euler equations are formulated in an integro-differential form for shape design sensitivity analysis and optimization. The principal tool employed to derive the performance derivative sensitivity equations is the variational method, which is a continuous alternat