Skip to content

Numath
- About Us
Research
People
Projects
Flow Databases
- Turbulent Channel Flow – ReT=200
- 2D cylinder – Re_D = 60
Tools
Publications
Events
Employment
Seminars

Menu

Numath
- About Us
Research
People
Projects
Flow Databases
- Turbulent Channel Flow – ReT=200
- 2D cylinder – Re_D = 60
Tools
Publications
Events
Employment
Seminars

Performance assessment of the controlled-diffusion S67B compressor cascade considering the influence of Reynolds number

September 16, 2019
10:34 pm

PrevPreviousEffect of Aspect Ratio on the Three-Dimensional Global Instability Analysis of Incompressible Open Cavity Flows

NextComputational analysis of the flow about a compressor stator cascade for gas turbine enginesNext

Some of our most representative Partners

Numath
Research
People
Projects
Publications
Events

Numath
Research
People
Projects
Publications
Events

Copyright 2023 | Numath | Numerical Methods in aerospace technology | All rights reserved.
Terms and Conditions | Privacy Policy | Cookie Policy