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个人简介
Professor Candler uses computational fluid dynamics to study high-temperature reacting flows and hypersonic flows, and is particularly interested in how the relaxation of internal energy modes and finite-rate chemical reactions interact with fluid motion. Applications of this work include the analysis of planetary entry spacecraft heat shields, hypersonic boundary layer transition, and the effects of chemical reactions on aerodynamics. Professor Candler works closely with experimentalists to validate high-enthalpy flow models by careful comparison to shock tunnel data. Recently, Candler's research group has been working to extend computational methods to complex geometries for application to future scramjet-powered hypersonic aircraft. These tools were used to design an inward-turning inlet for a upcoming sounding rocket flight experiment of a Mach 10 vehicle.
研究兴趣
论文共 537 篇作者统计合作学者相似作者
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AIAA SCITECH 2024 Forum (2024)
AIAA AVIATION FORUM AND ASCEND 2024 (2024)
Dale A. Lawrence,Brian M. Argrow,Joseph Pointer,Christopher Roseman, Nicholas Kenny, Joseph Habeck,James Flaten,Graham V. Candler,Aroh Barjatya, Julio Guardado
Journal of Spacecraft and Rocketspp.1-14, (2024)
AIAA SCITECH 2023 Forum (2023)
AIAA SCITECH 2023 Forum (2023)
AIAA AVIATION 2023 Forum (2023)
AIAA SCITECH 2023 Forum (2023)
AIAA SCITECH 2023 Forum (2023)
AIAA SCITECH 2023 Forum (2023)
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#Papers: 532
#Citation: 13777
H-Index: 51
G-Index: 96
Sociability: 7
Diversity: 0
Activity: 1
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