The Sectional Optimization Design of High Speed Aircraft at Ablation Thermal Protection
- Paper number
IAC-09.C2.6.8
- Author
Dr. Yin LianHua, China
- Year
2009
- Abstract
Ablation temperature software is developed. The structural size optimization of aircraft with ablation material protection is achieved. Thermal/aerodynamics load and only aerodynamics load with the effect of design result are compared.The result indicates that thermal-structural-aerodynamic coupling on multidisciplinary design optimization to high speed vechicle are necessary.
- Abstract document
- Manuscript document
(absent)