2022•Unpublished venueRequires access

Requirement Analysis and Design of a New Hyprsonic Aerodynamic Standard Model

Xiaobin Xu, Leitao Guo, Junbin Zhang, Feng Liu, Fei Xie

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Abstract

The development status of Chinese hypersonic aerodynamic standard model was described in this paper, the current development hotspot of hypersonic vehicle was summarized. The aerodynamic layout and characteristics of hypersonic aerodynamic standard model were briefly analyzed, and its deficiencies and limitations were also analyzed. The design requirements of hypersonic aerodynamics model were put forward, which can meet the development of aircraft at present and in the future. The wind tunnel test requirements of the new hypersonic aerodynamic model were analyzed, and two types of hypersonic vehicle model designs were identified. A new supermodel was designed which can reflect the typical characteristics of hypersonic vehicle such as aerodynamic layout, flow phenomenon and basic aerodynamic force.

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What this paper is about

The development status of Chinese hypersonic aerodynamic standard model was described in this paper, the current development hotspot of hypersonic vehicle was summarized. The aerodynamic layout and characteristics of hypersonic aerodynamic standard model were briefly analyzed, and its deficiencies and limitations were also analyzed. The design requirements of hypersonic aerodynamics model were put forward, which can meet the development of aircraft at present and in the future. The wind tunnel test requirements of the new hypersonic aerodynamic model were analyzed, and two types of hypersonic vehicle model designs were identified. A new supermodel was designed which can reflect the typical characteristics of hypersonic vehicle such as aerodynamic layout, flow phenomenon and basic aerodynamic force.

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Available abstract

The development status of Chinese hypersonic aerodynamic standard model was described in this paper, the current development hotspot of hypersonic vehicle was summarized. The aerodynamic layout and characteristics of hypersonic aerodynamic standard model were briefly analyzed, and its deficiencies and limitations were also analyzed. The design requirements of hypersonic aerodynamics model were put forward, which can meet the development of aircraft at present and in the future. The wind tunnel test requirements of the new hypersonic aerodynamic model were analyzed, and two types of hypersonic vehicle model designs were identified. A new supermodel was designed which can reflect the typical characteristics of hypersonic vehicle such as aerodynamic layout, flow phenomenon and basic aerodynamic force.

Key concepts: Aerodynamics, Hypersonic speed, Aerospace engineering, Computer science, Wind tunnel, Engineering

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