Aerodynamic optimization of the shape of supersonic compressor stage guide blades
Saved in:
Date: | 2017 |
---|---|
Main Authors: | Ju. A. Kvasha, N. A. Zinevich |
Format: | Article |
Language: | English |
Published: |
2017
|
Series: | Technical mechanics |
Online Access: | http://jnas.nbuv.gov.ua/article/UJRN-0000889461 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Journal Title: | Library portal of National Academy of Sciences of Ukraine | LibNAS |
Institution
Library portal of National Academy of Sciences of Ukraine | LibNASSimilar Items
-
On the effect of the tangential offset of blades on the power characteristics of the impeller of a supersonic compressor stage
by: Ju. A. Kvasha, et al.
Published: (2017) -
Aerodynamic optimisation of turbomachinery bladings: approaches, methods, results
by: S. V. Ershov, et al.
Published: (2012) -
The numerical analyzis for unsteady loads and elastic behaviour of the blades in seven stage axial compressor
by: L. V. Kolodjazhnaja
Published: (2011) -
The numerical analyzis for unsteady loads and elastic behaviour of the blades in seven stage axial compressor
by: Колодяжная, Л. В.
Published: (2016) -
The numerical analyzis for unsteady loads and elastic behaviour of the blades in seven stage axial compressor
by: Колодяжная, Л. В.
Published: (2016)