ANALYSIS AND TEST METHODS OF SUSPENSION STRUCTURE OF AIRBORNER MISSILE
The suspension structure is the key bearing structure of airborne missiles. In this paper, two methods are used to analyze the strength of the suspension structure. First, the inertia release method is used. This method can accurately simulate the boundary conditions of the hang up flight but the gr...
Saved in:
Main Authors: | SONG Lei, ZHANG Jin, WANG CongWei, JIN Ling, XU JunWei |
---|---|
Format: | Article |
Language: | zho |
Published: |
Editorial Office of Journal of Mechanical Strength
2019-01-01
|
Series: | Jixie qiangdu |
Subjects: | |
Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.03.042 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Comprehensive Review Comparing the Development and Challenges in the Energy Performance of Pneumatic and Hydropneumatic Suspension Systems
by: Ryszard Dindorf
Published: (2025-01-01) -
Absential Suspension: Malebranche and Locke on Human Freedom
by: Julie Walsh
Published: (2019-09-01) -
DYNAMIC PERFORMANCE ANALYSIS OF SCISSOR SEAT SUSPENSION SYSTEM
by: MA MingMing, et al.
Published: (2024-04-01) -
ROBUST OPTIMIZATION DESIGN OF SUSPENSION BASED ON 6σ
by: FENG JinZhi, et al.
Published: (2020-01-01) -
Development and Research of Fatigue Life Testing Device for Robot Reducer
by: Man Cheng, et al.
Published: (2019-05-01)