Non-probabilistic uncertainty analysis and optimization design method of multilayer thermal protection system based on experimental design

An uncertain and optimal design technology, applied in the field of optimal design of multi-layer thermal protection systems, can solve the problems of indistinguishable influence of temperature field response on thermophysical parameters, different heat transfer and heat storage efficiencies, and uncertainty of multi-layer thermal protection structures Analyzing Difficulties etc.

Active Publication Date: 2017-06-20
BEIHANG UNIV
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Problems solved by technology

However, the heat transfer and heat storage efficiencies of each layer structure are different and the layers are coupled with each other. It is difficult to distinguish the influen...

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  • Non-probabilistic uncertainty analysis and optimization design method of multilayer thermal protection system based on experimental design
  • Non-probabilistic uncertainty analysis and optimization design method of multilayer thermal protection system based on experimental design
  • Non-probabilistic uncertainty analysis and optimization design method of multilayer thermal protection system based on experimental design

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Embodiment Construction

[0028] The present invention proposes a non-probabilistic uncertainty analysis and optimal design method for multi-layer thermal protection systems based on experimental design. In order to fully understand the characteristics of the invention and its applicability to engineering practice, according to figure 1 The program flow shown realizes the optimal design of the multi-layer thermal protection system, including the following steps:

[0029] Step (1), according to the performance and configuration requirements determined by the actual service environment of the thermal protection system, the multi-layer thermal protection system is composed of 6 layers of different material structures with different functions, such as figure 2 As shown, from the outer surface to the inner surface, it includes a reinforced C / C layer, a room temperature curing adhesive layer, a high temperature insulation layer, a low temperature insulation layer, a strain isolation cushion layer and a skin ...

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Abstract

The invention discloses a non-probabilistic uncertainty analysis and optimization design method of a multilayer thermal protection system based on experimental design. The method comprises the following steps that (1) a thermal conductivity coefficient, density and specific heat capacity are selected as uncertain parameters to achieve an interval expression of each uncertain parameter; (2) thickness of each layer and the uncertain parameters are extracted as characteristic parameters to achieve fully parametric modeling, analyzing and solving; (3) a correlation of the uncertain parameters is considered, a random sampling method of correlation factors is put forward, and test samples are selected; (4) an approximate model is constructed according to the samples, influence of uncertain parameters on response is analyzed, optimization selection is carried out, and an uncertainty analysis method of a multilayer structure temperature field is established; (5) the thickness of each layer is taken as a design variable, the constraint condition is that temperature of each layer is smaller than an allowable value, quality minimization is taken as a target function, an optimization model is constructed, and the optimization design of the multilayer thermal protection system is achieved. According to the non-probabilistic uncertainty analysis and optimization design method of the multilayer thermal protection system based on the experimental design, and through efficient uncertainty analysis and optimization, the efficiency of a thermal protection system structure is improved.

Description

technical field [0001] The invention relates to the field of optimal design of a multi-layer thermal protection system, in particular to a method for non-probability uncertainty analysis and optimal design of a multi-layer thermal protection system based on test design. Background technique [0002] Due to the advantages of fast flight speed, short reaction time, large combat radius, good concealment, and strong defense penetration capabilities, hypersonic vehicles have a prominent position in the future war space and God's battlefield, and have become the world's major powers in the arms race. commanding heights. Hypersonic vehicles have been in service for a long time in the extreme environment of multi-field coupling dominated by aerodynamic heat and force, and thermal protection technology has become a bottleneck that directly restricts its development. In order to ensure the safety of pilots and the normal operation of airborne equipment, it is necessary to lay a large...

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Application Information

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IPC IPC(8): G06F17/50
CPCG06F30/15G06F30/23G06F2111/06G06F2111/08
Inventor 邱志平蒋文婷王晓军王睿星王磊石庆贺朱静静
Owner BEIHANG UNIV
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