...
首页> 外文期刊>Bioinspiration & biomimetics >The impact of dragonfly wing deformations on aerodynamic performance during forward flight
【24h】

The impact of dragonfly wing deformations on aerodynamic performance during forward flight

机译:蜻蜓翼变形对向前飞行期间空气动力学性能的影响

获取原文
获取原文并翻译 | 示例
           

摘要

Bulk wing kinematics and wing deformations of free-flying dragonflies of the species Pachydiplax longipennis were measured in a controlled environment. Both upright and inverted straight flights were recorded and analyzed. The inverted dragonflies exhibited similar bulk kinematics to the upright specimens in the global frame, but wing deformations were generally consistent in the body-relative frame. The deformations primarily comprised camber during the body-relative downstroke and twist during the body-relative upstroke. Based on these data, models were developed to incorporate the measured kinematics and deformations into computational fluid dynamics simulations. Both isolated and tandem wings were simulated (rigid and deforming in each case), allowing the effects of deformations and wing-wing interactions to be examined independently. During the upstroke the addition of deformation reduced flow separation on the outboard sections of the wing, whereas the impact of the deformation during the downstroke was found to be dependent on the wing kinematics. The simulations of tandem wings indicated that they produce more force than isolated wings, but the wing deformations reduced the impact of this wing-wing interaction. The changes in average lift and thrust induced by the wing deformations were relatively minor and dependent on the flight orientation, but the aerodynamic efficiency of the deforming wings was significantly higher than that of the rigid wings for all examined cases, including the inverted flights for which the deformations were in the opposite (global) sense to the upright flights.
机译:在受控环境中测量了物种Pachydiplax LongiPennis的自由飞行蜻蜓的散装翼运动学和机翼变形。记录和分析直立和倒立的直飞。倒蜻蜓在全球框架中的直立样本上表现出类似的散装运动学,但是翼变形通常在体相对框架中一致。变形主要包括在体内相对下午期间的弯曲和体内相对上行期间的扭曲。基于这些数据,开发了模型以将测量的运动学和变形掺入计算流体动力学模拟中。分离和串联翅膀被模拟(在每种情况下刚性和变形),允许独立地检查变形和翼翼相互作用的效果。在上行期间,在机翼的舷外部分上增加变形减小的流动分离,而在下游期间变形的影响是依赖于翼运动学。串联翅膀的模拟表明它们比隔离翼产生更多的力,但是机翼变形降低了这种翼翼相互作用的影响。由机翼变形引起的平均升力和推力的变化相对较小,取决于飞行方向,但变形翼的空气动力学效率显着高于所有检查案例的刚性翼的空气动力学效率,包括倒置飞行变形与直立飞行相反(全球)感。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号