Hybrid Wing-Body Pressurized Fuselage and Bulkhead, Design and Optimization.
作者:Mukhopadhyay, V. 加工时间:2014-09-03 信息来源:科技报告(NASA) 索取原文[14 页]
关键词:机身机翼结构;结构设计;固定机翼;复合材料结构 摘 要:The structural weight reduction of a pressurized Hybrid Wing-Body (HWB) fuselage is a serious challenge. Hence, research and development are presently being continued at NASA under the Environmentally Responsible Aviation (ERA) and Subsonic Fixed Wing.