Effects of Rotor-Bleeding Airflow on Aerodynamic and Structural Performances of a Single-Stage Transonic Axial Compressor
Crossref DOI link: https://doi.org/10.1007/s42405-019-00239-5
Published Online: 2019-12-20
Published Print: 2020-09
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Dinh, Cong-Truong http://orcid.org/0000-0001-5357-1534
Vu, Dinh-Quy
Kim, Kwang-Yong
Funding for this research was provided by:
National Foundation for Science and Technology Development (107.03-2018.20)
Text and Data Mining valid from 2019-12-20
Version of Record valid from 2019-12-20
Article History
Received: 4 August 2019
Revised: 13 November 2019
Accepted: 29 November 2019
First Online: 20 December 2019