Digital virtual flight testing and evaluation method for flight characteristics airworthiness compliance of civil aircraft based on HQRM
The authors are grateful to Dr. Xu Dongsong for joint research. They also thank the anonymous reviewers for their critical and constructive review of the manuscript. This study was supported by the National High-tech Research and Development Program of China 2014AA110500
2015-03-25(万方平台首次上网日期,不代表论文的发表时间)
共9页
112-120