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http://dx.doi.org/10.5139/JKSAS.2019.47.10.695

A Study on the Structural Integrity of Hypersonic Vehicles According to Flight Conditions  

Kang, Yeon Cheol (Department of Aerospace Engineering, Inha University)
Kim, Gyubin (Department of Aerospace Engineering, Inha University)
Kim, Jeong Ho (Department of Aerospace Engineering, Inha University)
Cho, Jin Yeon (Department of Aerospace Engineering, Inha University)
Kim, Heon Ju (Agency for Defense Development)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.47, no.10, 2019 , pp. 695-704 More about this Journal
Abstract
In hypersonic regime, the complicated interaction between the air and surface of aircraft results in intensive aerodynamic heating on body. Provided this phenomenon occurs on a hypersonic vehicle, the temperature of the body extremely increases. And consequently, thermal deformation is produced and material properties are degraded. Furthermore, those affect both the aerothermoelastic stability and thermal safety of structures significantly. With the background, thermal safety and dynamic stability are studied according to the altitude, flight time and Mach number. Based on the investigation, design guideline is suggested to guarantees the structural integrity of hypersonic vehicles in terms of both of thermal safety and dynamic stability.
Keywords
Aero-thermo-elastic Analysis; Hypersonic; Flutter; Thermal Safety; Diagram-based Method;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
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