Test section of the wind tunnel IT for aeroelastic experiments with blade cascades
The article presents the way how the existing small vacuum aerodynamic tunnel IT (Institute of Thermomechanics) has been adapted for the measurement of the aeroelastic properties of the NACA 0015 airfoil and of the blade cascades composed of various types of blades with two degrees of freedom, pitch...
Main Authors: | Vlček Václav, Procházka Pavel |
---|---|
Format: | Article |
Language: | English |
Published: |
EDP Sciences
2019-01-01
|
Series: | EPJ Web of Conferences |
Online Access: | https://www.epj-conferences.org/articles/epjconf/pdf/2019/18/epjconf_efm18_02095.pdf |
Similar Items
-
Evaluation of a subsonic cascade wind tunnel for compressor blade testing.
by: DuVal, David A.
Published: (2012) -
Cascade wind tunnel for transonic compressor blading studies.
by: Demo, Willard Joe
Published: (2012) -
Numerical Investigation of Aeroelastic Flutter in Two-Dimensional Cascade of Compressor Blades
by: Fürst Jiří, et al.
Published: (2020-01-01) -
Subsonic cascade wind tunnel tests using a compressor configuration of DCA blades.
by: Cina, Frank S.
Published: (2012) -
Sensitivity Study of the Influence of Blade Sectional Stiffness Parameters on the Aeroelastic Response of Wind Turbines
by: Cheng Chen, et al.
Published: (2021-08-01)