Details
| Titel in Übersetzung | 基于等几何分析的太阳帆板热结构耦合随机动力响应 |
|---|---|
| Originalsprache | Mehrere Sprachen |
| Aufsatznummer | 722338 |
| Fachzeitschrift | Acta Mechanica Sinica/Lixue Xuebao |
| Jahrgang | 39 |
| Ausgabenummer | 4 |
| Frühes Online-Datum | 20 Apr. 2023 |
| Publikationsstatus | Veröffentlicht - Apr. 2023 |
Abstract
The spacecraft experiences changes of light region periodically and will be seriously affected by the thermal stress caused by the solar radiation. Based on the isogeometric analysis, the random dynamic responses of solar array with random field parameters under thermal-structural coupling are addressed. Firstly, the heat conduction differential equation and vibration differential equation of the solar array are obtained based on the geometric model constructed with non-uniform rational B-spline. The differential equations under thermal-structural coupling are then solved by using Newmark-β method to obtain the structural temperature field and the random dynamic responses. Finally, the influences of different random field parameters on structural dynamic response are investigated. [Figure not available: see fulltext.]
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Numerische Mechanik
- Ingenieurwesen (insg.)
- Maschinenbau
Zitieren
- Standard
- Harvard
- Apa
- Vancouver
- BibTex
- RIS
in: Acta Mechanica Sinica/Lixue Xuebao, Jahrgang 39, Nr. 4, 722338, 04.2023.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - Random dynamic responses of solar array under thermal-structural coupling based on the isogeometric analysis
AU - Ma, Juan
AU - Dai, Changping
AU - Wang, Bo
AU - Beer, Michael
AU - Wang, Anyi
N1 - Funding Information: This work was supported by the National Natural Science Foundation of China (Grant No. 11572233) and the National Defense Pre-Research Foundation of China (Grant No. 61400020106) as well as the Fundamental Research Funds for the Central Universities.
PY - 2023/4
Y1 - 2023/4
N2 - The spacecraft experiences changes of light region periodically and will be seriously affected by the thermal stress caused by the solar radiation. Based on the isogeometric analysis, the random dynamic responses of solar array with random field parameters under thermal-structural coupling are addressed. Firstly, the heat conduction differential equation and vibration differential equation of the solar array are obtained based on the geometric model constructed with non-uniform rational B-spline. The differential equations under thermal-structural coupling are then solved by using Newmark-β method to obtain the structural temperature field and the random dynamic responses. Finally, the influences of different random field parameters on structural dynamic response are investigated. [Figure not available: see fulltext.]
AB - The spacecraft experiences changes of light region periodically and will be seriously affected by the thermal stress caused by the solar radiation. Based on the isogeometric analysis, the random dynamic responses of solar array with random field parameters under thermal-structural coupling are addressed. Firstly, the heat conduction differential equation and vibration differential equation of the solar array are obtained based on the geometric model constructed with non-uniform rational B-spline. The differential equations under thermal-structural coupling are then solved by using Newmark-β method to obtain the structural temperature field and the random dynamic responses. Finally, the influences of different random field parameters on structural dynamic response are investigated. [Figure not available: see fulltext.]
KW - Isogeometric analysis
KW - Non-uniform rational B-spline
KW - Random dynamic responses
KW - Random field parameters
KW - Thermal-structural coupling
UR - http://www.scopus.com/inward/record.url?scp=85156194270&partnerID=8YFLogxK
U2 - 10.1007/s10409-023-22338-x
DO - 10.1007/s10409-023-22338-x
M3 - Article
AN - SCOPUS:85156194270
VL - 39
JO - Acta Mechanica Sinica/Lixue Xuebao
JF - Acta Mechanica Sinica/Lixue Xuebao
SN - 0567-7718
IS - 4
M1 - 722338
ER -