Vibration Test of Blade Discof High Pressure Turbine in High Rotating Speed

doi:10.16615/j.cnki.1674-8190.2021.01.011

Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University

Home > Archive>Volume 12, Issue 1, 2021 >85-90. DOI:10.16615/j.cnki.1674-8190.2021.01.011

PDF HTML XML Export Cite reminder

Vibration Test of Blade Discof High Pressure Turbine in High Rotating Speed
DOI:
                        10.16615/j.cnki.1674-8190.2021.01.011
                    
Author:
                        
                        
                    
Affiliation:1.AECC Commercial Aircraft Engine Co., Ltd;2.Shanghai Commercial Aircraft Engine Engineering Technology Research Center
Clc Number:V232.4
Fund Project:

Article

Figures

Metrics

Reference

Cited by

Materials

Comments

Abstract:

Reference

Cited by

Get Citation

luoli, huang da yong. Vibration Test of Blade Discof High Pressure Turbine in High Rotating Speed[J]. Advances in Aeronautical Science and Engineering,2021,12(1):85-90

Copy

Article Metrics

Abstract:
PDF:
HTML:
Cited by:

History

Received:March 12,2020
Revised:May 07,2020
Adopted:May 24,2020
Online: February 25,2021
Published:

Get Citation

Share

Article Metrics

History