Aerohydrodynamics of flapping-wing propulsors

被引:180
|
作者
Rozhdestvensky, KV [1 ]
Ryzhov, VA [1 ]
机构
[1] St Petersburg State Marine Tech Univ, Dept Appl Math & Math Modeling, St Petersburg 190008, Russia
关键词
D O I
10.1016/S0376-0421(03)00077-0
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
It is the objective of this survey to review research and development results of flapping-wing propulsors and of vehicles equipped with them. Given the complex and multi-disciplinary character of the problem, a wide range of questions is considered in order to provide a general idea of the state-of-the-art. The main attention is directed at the aerohydrodynamics of flapping-wing propulsors. The major relevant mathematical models and the corresponding numerical results are presented together with the experimental data obtained up to the present time. Also, the physical and the design factors are discussed, which affect the aerohydrodynamic characteristics of flapping wings and that therefore have to be accounted for in the modern mathematical models. Experimental data and numerical modeling results are compared to determine domains of validity of the latter for the aerohydrodynamic design of full-scale air and marine vehicles. Also, existing engineering solutions for vehicles with flapping-wing propulsors are presented and prospective directions for future investigations are outlined. (C) 2003 Elsevier Ltd. All rights reserved.
引用
收藏
页码:585 / 633
页数:49
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