A Three-Dimensional Actuator Disk Model for Fan Response to Inlet Distortion: Part II - Applications
Year: 2025
Type: article
Source: Journal of Turbomachinery
DOI: 10.1115/1.4069510
Author: Dilip Prasad
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4413350451
