Design of High Altitude Propeller Using Multilevel Optimization

DOI10.1142/S021987621950004XzbMath1476.74123WikidataQ128766738 ScholiaQ128766738MaRDI QIDQ5207372

Weiliang He, Fengmei Wei, Xinqiang Liu

Publication date: 20 December 2019

Published in: International Journal of Computational Methods (Search for Journal in Brave)

zbMATH Keywords

NSGA-IImultilevel optimizationCFD simulationblade element momentum theoryhigh altitude propellerMIGA

Mathematics Subject Classification ID

Compliance or weight optimization in solid mechanics (74P05)

Related Items (2)

A Multi-Dimensional Lagrange Multiplier Method to Identify the Load Distribution on 3D Special-Shaped Surface in the Strength Analysis of Aircraft Structure ⋮ An Ecological Equilibrium Dynamics Optimization Approach

Uses Software

• XFOIL

Cites Work

• A Comparison of Three Methods for Selecting Values of Input Variables in the Analysis of Output from a Computer Code
• Numerical Investigation of Different Tip Clearances Effect on the Hydrodynamic Performance of Pumpjet Propulsor
• APPLICATION OF A PRESSURE CORRECTION METHOD FOR MODELING INCOMPRESSIBLE FLOW THROUGH TURBOMACHINES

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