Numerical and Theoretical Investigations Concerning the Continuous-Surface-Curvature Effect in Compressor Blades
Though the importance of curvature continuity on compressor blade performances has been realized, there are two major questions that need to be solved, i.e., the respective effects of curvature continuity at the leading-edge blend point and the main surface, and the contradiction between the traditi...
Main Authors: | Yin Song, Chun-Wei Gu, Yao-Bing Xiao |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2014-12-01
|
Series: | Energies |
Subjects: | |
Online Access: | http://www.mdpi.com/1996-1073/7/12/8150 |
Similar Items
-
Impact of leading-edge orientation and shape on performance of a compressor blade
by: Powell, Jonathan D.
Published: (2012) -
Numerical prediction of the impact of non-uniform leading edge coatings on the aerodynamic performance of compressor airfoils
by: Elmstrom, Michael E.
Published: (2012) -
Development of a Preliminary Design Method for Subsonic Splittered Blades in Highly Loaded Axial-Flow Compressors
by: Baojie Liu, et al.
Published: (2017-03-01) -
A numerical solution of implicit nonlinear equations of motion for rotor blades
by: Kim, Young K.
Published: (2006) -
QUASI THREE DIMENSIONAL COMPRESSOR DESIGN FOR A TWIN-SPOOL LOW BYPASS RATIO TURBOFAN ENGINE
by: Serdar Duman, et al.
Published: (2012-01-01)