Mitigation of Circumferential Inlet Distortion Effects Using Non-Axisymmetric Fan Inlet and Exit Guide Vanes
Year: 2025
Type: article
Source: Journal of Turbomachinery
DOI: 10.1115/1.4072203
Authors: Michael A. Kramer, David K. Hall
Institution: Pennsylvania State University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4413218039
