Work

Supersonic Aircraft Drag Reduction Optimization Design in a Wide Speed Range Based on the Adjoint Method

Year: 2024

Type: conference-paper

DOI: 10.1109/meae62008.2024.11026549

Authors: Luo Xiao, Song Chao, Liu Hongyang, Zhou Zhu, Tang Yu

Institution: China Aerodynamics Research and Development Center

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4411409505

FWCI:

Cites: 18

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Related to: 10