Validation of comprehensive dynamics analysis predictions for a rotor in descending flight

Abstract

Purpose

The purpose of this paper is to evaluate the prediction capability of comprehensive structural dynamics (CSD) analysis codes for the higher harmonic control aeroacoustic rotor test (HART) II data.

Design/methodology/approach

A nonlinear flexible multibody dynamics analysis code DYMORE, as well as the comprehensive analytical model of rotorcraft aerodynamics and dynamics (CAMRAD) II, are used to perform the task. The predicted results on rotating free vibration analysis, airloads, blade elastic motions, and structural moments are correlated with the measured data for the baseline, minimum noise, and minimum vibration cases.

Findings

The DYMORE analysis results with a free wake model show a good performance in capturing blade vortex interaction peaks in the prediction of section normal forces but apparently with a phase shift problem. The high‐frequency behavior in the airloads signal does not affect much on the aeroelastic response and structural moments of the rotor.

Originality/value

The present approach uses two separate CSD codes to systematically validate the HART II data. The accuracy of each code on structural dynamic aspects of HART II rotor is assessed using a consistent set of inputs. The effects of blade tip deflections on the interaction of blades and their trailed vortices leading to a reduced noise emission are also investigated.

Citation

Park, J.S., Jung, S.N., You, Y.H., Park, S.H. and Yu, Y.H. (2011), "Validation of comprehensive dynamics analysis predictions for a rotor in descending flight", Aircraft Engineering and Aerospace Technology, Vol. 83 No. 2, pp. 75-84. https://doi.org/10.1108/00022661111120962