Post by Steve Yenisch on May 14, 2009 11:40:03 GMT -5
Paper: dl.getdropbox.com/u/473092/WCSMO8.pdf
Presentation: www.mae.ufl.edu/nkim/ISSMO/Diane_internetconf.htm
ABSTRACT
Space vehicles traveling at hypersonic speeds through a planetary atmosphere experience severe aerodynamic heating. An integrated thermal protection system (ITPS) serves to protect the vehicle from this aerodynamic heating, while also providing some structural load bearing function. The design of an ITPS is a compromise between structural requirements of robust structural members and the need to limit the heat conducted through these members. This compromise is an exercise in risk allocation between structural and thermal failures.
In deterministic approaches, risk allocation between failure modes is implicit in the choice of safety factors and margins. Probabilistic optimization can be used to allocate risk explicitly between failure modes. Previous work has shown the differences in risk allocation between deterministic and probabilistic optimization with constraints on the maximum temperature and buckling of the ITPS web. In this study, the effect of addition of a constraint on the maximum von Mises stress in the web on the risk allocation is examined. The ABAQUS finite element program is used to generate transient thermal response under reentry heating loads, and the structural response is calculated at critical times (e.g., time at which temperature gradient is maximum) during the re-entry process. Separable Monte Carlo is used to evaluate the limit states corresponding to the three failure modes. Probabilistic optimization reduced the mass of the ITPS by 1.2% while maintaining the same level of reliability as the deterministic design. More risk was allocated to thermal and stress failures after optimization and the probability of buckling failure was greatly reduced. The presence of only a few combined thermal-stress and buckling-stress failure modes were noted in the deterministic design, and even fewer were found in the probabilistic design.
Presentation: www.mae.ufl.edu/nkim/ISSMO/Diane_internetconf.htm
Risk Allocation by Optimization of an Integrated Thermal Protection System
Diane Villanueva1, Anurag Sharma2, Raphael T. Haftka3, Bhavani V. Sankar4
1 Graduate Research Assitant, University of Florida, Gainesville, FL, U.S.A
tanfoudy@ufl.edu
2 PhD Candidate, University of Florida, Gainesville, FL, U.S.A
anurag46@ufl.edu
3 Distinguished Professor, University of Florida, Gainesville, FL, U.S.A
haftka@ufl.edu
4 Ebaugh Professor, University of Florida, Gainesville, FL, U.S.A
sankar@ufl.edu
Diane Villanueva1, Anurag Sharma2, Raphael T. Haftka3, Bhavani V. Sankar4
1 Graduate Research Assitant, University of Florida, Gainesville, FL, U.S.A
tanfoudy@ufl.edu
2 PhD Candidate, University of Florida, Gainesville, FL, U.S.A
anurag46@ufl.edu
3 Distinguished Professor, University of Florida, Gainesville, FL, U.S.A
haftka@ufl.edu
4 Ebaugh Professor, University of Florida, Gainesville, FL, U.S.A
sankar@ufl.edu
ABSTRACT
Space vehicles traveling at hypersonic speeds through a planetary atmosphere experience severe aerodynamic heating. An integrated thermal protection system (ITPS) serves to protect the vehicle from this aerodynamic heating, while also providing some structural load bearing function. The design of an ITPS is a compromise between structural requirements of robust structural members and the need to limit the heat conducted through these members. This compromise is an exercise in risk allocation between structural and thermal failures.
In deterministic approaches, risk allocation between failure modes is implicit in the choice of safety factors and margins. Probabilistic optimization can be used to allocate risk explicitly between failure modes. Previous work has shown the differences in risk allocation between deterministic and probabilistic optimization with constraints on the maximum temperature and buckling of the ITPS web. In this study, the effect of addition of a constraint on the maximum von Mises stress in the web on the risk allocation is examined. The ABAQUS finite element program is used to generate transient thermal response under reentry heating loads, and the structural response is calculated at critical times (e.g., time at which temperature gradient is maximum) during the re-entry process. Separable Monte Carlo is used to evaluate the limit states corresponding to the three failure modes. Probabilistic optimization reduced the mass of the ITPS by 1.2% while maintaining the same level of reliability as the deterministic design. More risk was allocated to thermal and stress failures after optimization and the probability of buckling failure was greatly reduced. The presence of only a few combined thermal-stress and buckling-stress failure modes were noted in the deterministic design, and even fewer were found in the probabilistic design.