Development of deployable wing glider

• المؤلف الرئيسي: Lim, Bi Fang.
• مؤلفون آخرون: Murukeshan Vadakke Matham
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2013
• الموضوعات: DRNTU::Engineering
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/53541

This report will explore the development of a deployable wing mechanism for use in gliders of wingspan 1-1.5 metres. The wing will be stowed along the fuselage prior to launch and will be deployed to its desired location in flight. The objective of wing stowage is to achieve a higher height attainme...