Work

Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method

Year: 2024

Type: article

Source: Journal of Turbomachinery

DOI: 10.1115/1.4067290

Authors: Hangkong Wu, Dingxi Wang, Xiuquan Huang

Institutions: Northwestern Polytechnical University, San Francisco Bay University

Language: English

Topic: Turbomachinery Performance and Optimization

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funders: Northwestern Polytechnical University, Aeronautical Science Foundation of China, Aerostatic Science Foundation

Award: G8750386227

OpenAlex ID: W4404759807

FWCI: 0.534

Cites: 34

Cited by: 3

Related to: 10