Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure
Joint Authors
Zhang, Zhiyuan
Chi, Runqiang
Pang, Baojun
Guan, Gongshun
Source
International Journal of Aerospace Engineering
Issue
Vol. 2017, Issue 2017 (31 Dec. 2017), pp.1-9, 9 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2017-04-16
Country of Publication
Egypt
No. of Pages
9
Abstract EN
In the present study, the microspacecraft bulkhead was reduced to the double honeycomb panel, and the projectile oblique hypervelocity impact on the double honeycomb panel was simulated.
The distribution of the debris cloud and the damage of a honeycomb sandwich panel were investigated when the incident angles were set to be 60°, 45°, and 30°.
The results showed that as incident angle decreased, the distribution of debris cloud was increased gradually, while the maximum perforation size of the rear face sheet was firstly increased with the decrease of the incident angle and then decreased.
On the other hand, the damage area and the damage degree of the front face sheet of the second honeycomb panel layer were increased with the decrease of the incident angle.
Finally, the critical angle of front and rear face sheets of the honeycomb sandwich panel was obtained under oblique hypervelocity impact.
American Psychological Association (APA)
Zhang, Zhiyuan& Chi, Runqiang& Pang, Baojun& Guan, Gongshun. 2017. Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure. International Journal of Aerospace Engineering،Vol. 2017, no. 2017, pp.1-9.
https://search.emarefa.net/detail/BIM-1157729
Modern Language Association (MLA)
Zhang, Zhiyuan…[et al.]. Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure. International Journal of Aerospace Engineering No. 2017 (2017), pp.1-9.
https://search.emarefa.net/detail/BIM-1157729
American Medical Association (AMA)
Zhang, Zhiyuan& Chi, Runqiang& Pang, Baojun& Guan, Gongshun. Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure. International Journal of Aerospace Engineering. 2017. Vol. 2017, no. 2017, pp.1-9.
https://search.emarefa.net/detail/BIM-1157729
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1157729