Dynamics models of flexible aircraft

• المؤلف الرئيسي: Yogeshwaran Jayaraman
• مؤلفون آخرون: Hungsun Son
• التنسيق: Theses and Dissertations
• اللغة: English
• منشور في: 2014
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Flight simulation; DRNTU::Engineering::Aeronautical engineering::Aircraft
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/61444

Recent trends in aircraft design owing to requirements of high performance and weight reduction have resulted in aircraft possessing significant structural flexibility. Under these conditions, flight vehicles become vulnerable to unfavourable interactions between the structural dynamics of flexible...