Conceptual design of UAV airframes using a generic geometry service
暂无分享,去创建一个
With the increased freedom in layout selection possible when designing an Unmanned Air Vehicle (UAV) concept (compared, for example, to the relatively constrained and mature world of commercial airliner design), comes the significant challenge of building a geometry engine that will provide the variety of airframe models demanded by the highly global nature of the design search. In order to enable multidisciplinary trade-off studies, both an external surface and an internal structure are required – we use a single, generic model to supply these, in the form of a parametric geometry residing in a commercial
CAD tool. In addition to discussing the challenges of offering a truly flexible geometry service, we also delve into the UAV-specific issues of the initial sizing of the model. A wealth of statistical data provides one of the traditional handholds for this step in manned aircraft conceptual design – we discuss the
applicability of such statistical approaches to their unmanned counterparts.
[1] Daniel P. Raymer,et al. Aircraft Design: A Conceptual Approach , 1989 .
[2] D. R. Haddon,et al. Aircraft Airworthiness Certification Standards for Civil UAVs , 2003 .
[3] J. Samareh. Survey of Shape Parameterization Techniques for High-Fidelity Multidisciplinary Shape Optimization , 2001 .