Study on Landing Gear’s Load for Airship Based on the Double-springs’ Vibration Model
The FAA-P-8110-2 Airship Design Criteria defines the airworthiness standard requirement. In order to make the design of landing gear to fulfill the requirements perfectly, a methodology of load calculation for landing gear is presented in this paper, which is based on double-springs’ vibration model...
| 出版年: | Hangkong gongcheng jinzhan |
|---|---|
| 主要な著者: | , , |
| フォーマット: | 論文 |
| 言語: | 中国語 |
| 出版事項: |
Editorial Department of Advances in Aeronautical Science and Engineering
2020-12-01
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| 主題: | |
| オンライン・アクセス: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2020129?st=article_issue |
