Research on the Status and Key Technology of Adaptive Wings

doi:10.16615/j.cnki.1674-8190.2018.03.001

Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University

Home > Archive>Volume 9, Issue 3, 2018 >297-308. DOI:10.16615/j.cnki.1674-8190.2018.03.001

PDF HTML XML Export Cite reminder

Research on the Status and Key Technology of Adaptive Wings
DOI:
                        10.16615/j.cnki.1674-8190.2018.03.001
                    
Author:
                        
                        
                    
Affiliation:Aircraft Strength Research Institute of China,Aircraft Strength Research Institute of China
Clc Number:V271.4
Fund Project:

Article

Figures

Metrics

Reference

Cited by

Materials

Comments

Abstract:

This paper focuses on the research on the status of adaptive wing and summarizes from the adaptive compliant leading edge, the adaptive compliant trailing edge and the variable thickness wing, respectively. And the key technology that adaptive wing needs to be solved urgently is put forward, which can provide some technical reference for the design and implementation of adaptive wing structure.

Reference

Cited by

Get Citation

NI Ying-ge, YANG Yu. Research on the Status and Key Technology of Adaptive Wings[J]. Advances in Aeronautical Science and Engineering,2018,9(3):297-308

Copy

Article Metrics

Abstract:
PDF:
HTML:
Cited by:

History

Received:November 01,2017
Revised:December 12,2017
Adopted:January 12,2018
Online: July 16,2018
Published:

Get Citation

Share

Article Metrics

History