Investigation of 3-D strains on highly-twisted swept tip composite rotor blades

Chi, Cheng; Datta, Anubhav; Chopra, Inderjit

Abstract

This paper presents an investigation of the effects of swept tip on highly twisted composite rotor blades. The focus is on detailed three dimensional (3-D) strain measurement. Both vacuum chamber tests and 3-D finite element method (FEM) analysis were carried out in the investigation. Strain distribution on three sets of in-house fabricated composite blades: straight, twisted, and twisted-swept were studied using strain gauges in a rotating environment in a vacuum chamber. A set of aluminum beams were also tested as an elementary baseline to aid in fundamental understanding. A prediction study of 3-D strain patterns were conducted by X3D: a 3-D structural dynamic solver. Correlating measured strains with the predictions showed overall good agreements. Evidences of strong lead-lag bending moment counteracting the axial extension are found in both aluminum beams and composite blades. Strain patterns of aluminum beams and composite blades have some superficial similarities, but they are not the same. An in-plane shear strain concentration is an unique phenomenon in the swept tip composite blades.

• Presentation Conference Type: Conference Paper (published)
• Conference Name: Vertical Flight Society 75th Annual Forum & Technology Display
• Start Date: May 13, 2019
• End Date: May 16, 2019
• Online Publication Date: May 13, 2019
• Publication Date: May 13, 2019
• Deposit Date: Dec 19, 2024
• Peer Reviewed: Peer Reviewed
• Pages: 1-16
• DOI: https://doi.org/10.4050/f-0075-2019-14743
• Public URL: https://uwe-repository.worktribe.com/output/13537746