The 5-dimensional liquid hydrogen tank problem is a reliability analysis benchmark problem (Bichon et al., 2011). The problem consists in quantifying the failure probability of a liquid hydrogen fuel tank on a space launch vehicle. The structure of the tank is subjected to stresses caused by ullage pressure, head pressure, axial forces due to acceleration, and bending and shear stresses caused by the weight of the fuel.
Description
Three different failure modes exist for the tank:
- Von Mises stress failure (P_{VM})
- Isotropic strength failure (P_{IS})
- Honeycomb buckling failure (P_{HB})
The limit state function of the overall system is then defined as:
where:
and:
- x_1 = 4 (t_{\text{plate}} - 0.075)
- x_2 = 20 (t_h - 0.1)
- x_3 = -6 \cdot 10^3 (\frac{1}{N_{xy}} + 0.003)
while the input variables of the performance function are \mathbf{x} = \{t_{\text{plate}}, t_{h}, N_x, N_y, N_{xy}\}.
The failure event is defined as g(\mathbf{x}) \leq 0 and the failure probability P_f = \mathbb{P}[g(\mathbf{x}) \leq 0].
Inputs
The five input variables are modeled as independent Gaussian random variables.
No | Variable | Distribution | Parameters | Description |
---|---|---|---|---|
1 | t_{\text{plate}} | Gaussian |
\mu_{t_\text{plate}} = 0.07433 \sigma_{t_\text{plate}} = 0.005 |
Plate thickness |
2 | t_{h} | Gaussian |
\mu_{t_h} = 0.1 \sigma_{t_h} = 0.01 |
Honeycomb thickness |
3 | N_x | Gaussian |
\mu_{N_x} = 13 \sigma_{N_x} = 60 |
Load on tank, x-component |
4 | N_y | Gaussian |
\mu_{N_y} = 4751 \sigma_{N_y} = 48 |
Load on tank y-component |
5 | N_{xy} | Gaussian |
\mu_{N_{xy}} = -648 \sigma_{N_{xy}} = 11 |
Load on tank xy-component |
Reference values
Some reference values for the failure probability P_f from the literature are shown in the table below. Note that the values from Bichon et al. (2011) are average values over 20 replications.
Method | N | \hat{P_f} | \text{CoV}[\hat{P_f}] | Source |
---|---|---|---|---|
MCS (LHS) | 10^4 | 7.0 \times 10^{-4} | - | Bichon et al. (2011) |
MCS (LHS) | 10^5 | 6.92 \times 10^{-4} | - | Bichon et al. (2011) |
MCS (LHS) | 10^6 | 6.97 \times 10^{-4} | - | Bichon et al. (2011) |
MCS | 10^6 | 7.1 \times 10^{-4} | 3.75\% | UQLab v1.2.1 |
Resources
The vectorized implementation of the limit state function for the liquid hydrogen tank problem in MATLAB as well as the script file with the model and probabilistic inputs definitions for the function in UQLAB can be downloaded below:
uq_liquidHydrogenTank.zip (3.0 KB)
The contents of the file are:
Filename | Description |
---|---|
uq_liquidHydrogenTank.m |
vectorized implementation of the limit state function of the liquid hydrogen tank problem in MATLAB |
uq_Example_liquidHydrogenTank.m |
definitions for the model and probabilistic inputs in UQLab |
LICENSE |
license for the function (BSD 3-Clause) |
References
- B. J. Bichon, J. M. McFarland, and S. Mahadevan, “Efficient surrogate models for reliability analysis of systems with multiple failure modes,” Reliability Engineering & System Safety, vol. 96, no. 10, pp. 1386-1395, 2011. DOI:10.1016/j.ress.2011.05.008