Parameter resembling method for aerodynamic thermal environment experimental simulation conditions

A technology for simulating conditions and environmental tests, applied in the aerospace field, can solve problems such as high test costs and large deviations in flight status, and achieve the effect of broadening test simulation conditions
CN109029907AActive Publication Date: 2018-12-18DALIAN UNIV OF TECH
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Patent Information

Authority / Receiving Office
CN Β· China
Patent Type
Applications(China)
Current Assignee / Owner
DALIAN UNIV OF TECH
Publication Date
2018-12-18

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Abstract

The invention belongs to the technical field of aerospace, and relates to a parameter resembling method for aerodynamic thermal environment experimental simulation conditions. According to the requirement of equivalence of recovery enthalpy and cold wall heatflow in an aerodynamic thermal environment experiment, a method of guaranteeing ground test parameters being similar to flight parameters without recovery enthalpy equivalence, and the problems at the present stage that experimental simulation method depends on recovery enthalpy equivalence and accurate simulation of the real aerodynamic heat environment is difficult are solved. A guarantee for heat transfer and ablation experimental study of thermal shielding / insulation material in the high temperature aerodynamic thermal environmentis provided. The parameter resembling method has the beneficial effects that experimental conditions are not affected by recovery enthalpy value; most test equipment can simulate the high enthalpy aerodynamic thermal environment; a new way of parameter adjustment for high enthalpy wind tunnel testing is provided; and the experimental simulation conditions are broadened.
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Description

technical field

[0001] The invention belongs to the field of aerospace technology, and relates to a test simulation method for the aerodynamic thermal environment of an anti / heat insulation material, in particular to a parameter similar method for high-temperature aerodynamic thermal environment simulation test conditions when it is difficult to ensure that the recovery enthalpy and cold wall heat flow are equal at the same time. Background technique

[0002] When the aircraft flies at supersonic speed and hypersonic speed, it will face extremely harsh aerothermal environment and be subjected to strong aerodynamic heat and aerodynamic force. In order to study the working state of the aircraft's external heat protection structure in a complex aerodynamic and thermal environment, it is necessary to simulate the real aerodynamic and thermal environment of the aircraft through ground tests, and to evaluate the performance indicators of the thermal protection structure materials, ...

Claims

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