Design and test of synthetic jet actuator for propulsion

• المؤلف الرئيسي: Teo, Nathaniel Desheng
• مؤلفون آخرون: Tang Chuyang
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2014
• الموضوعات: DRNTU::Engineering
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/60934
• المؤسسة: Nanyang Technological University

Compact zero-mass pulsatile jet actuators are proposed for low speed maneuvering and station keeping of small, autonomous underwater vehicles. Hence, the optimization of synthetic jets for maximal thrust generation is being investigated. Flow field of such jets are initially dominated by vortex ring...