Aerothermodynamic Optimization of Aerospace Plane Airfoil Leading Edge

Aerothermodynamic Optimization of Aerospace Plane Airfoil Leading Edge

Aiming to mitigate the aerodynamic heating during hypersonic re-entry, the aerothermodynamic optimization of aerospace plane airfoil leading edge is conducted. Lift-todrag ratio at landing condition is taken as a constraint to ensure the landing aerodynamic performance. First, airfoil profile is par...

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Bibliographic Details
Main Authors: Chen Zhou, Zhijin Wang, Jiaoyang Zhi, Anatolii Kretov
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2017-10-01
Series:Journal of Aerospace Technology and Management
Subjects:
Airfoil optimization
Aerodynamic heating
Hicks-Henne type function
Airfoil parameterization
Surrogate model.
Online Access:https://www.jatm.com.br/jatm/article/view/820

Internet

https://www.jatm.com.br/jatm/article/view/820

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