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A Technique for Stress-Strain State Analysis, Optimization and Experimental Study of a Hybrid Composite-Metal Propeller Blade.
- Source :
- Russian Aeronautics; Apr2022, Vol. 65 Issue 2, p260-267, 8p
- Publication Year :
- 2022
-
Abstract
- This paper presents a technique for stress-strain state analysis, optimization and experimental study of the stiffness of a hybrid composite-metal propeller blade. It demonstrates the results of numerical and experimental study and presents the stresses and total displacements of all hybrid blade elements. [ABSTRACT FROM AUTHOR]
Details
- Language :
- English
- ISSN :
- 10687998
- Volume :
- 65
- Issue :
- 2
- Database :
- Complementary Index
- Journal :
- Russian Aeronautics
- Publication Type :
- Academic Journal
- Accession number :
- 162260587
- Full Text :
- https://doi.org/10.3103/S1068799822020052