Strathprints logo
Strathprints Home | Open Access | Browse | Search | User area | Copyright | Help | Library Home | SUPrimo

The effect of blade aerodynamic modelling on the prediction of the blade airloads and the acoustic signature of the HART II rotor

Kelly, Mary E. and Brown, R.E. (2009) The effect of blade aerodynamic modelling on the prediction of the blade airloads and the acoustic signature of the HART II rotor. In: 35th European Rotorcraft Forum, 2009-09-22 - 2009-09-25, Hamburg, Gemany.

[img]
Preview
PDF (strathprints027437.pdf)
strathprints027437.pdf

Download (4MB) | Preview

Abstract

As a rotorcraft descends or manoeuvres, the interactions which occur between the rotor blades and vortical structures within the rotor wake produce highly impulsive loads on the blades and with these a highly intrusive external noise. Brown's Vorticity Transport Model has been used to investigate the influence of the fidelity of the local blade aerodynamic model on the quality of the prediction of the high-frequency airloads associated with blade-vortex interactions and thus on the accuracy with which the acoustic signature of the aircraft can be predicted. The Vorticity Transport Model can resolve very accurately the structure of the wake, and allows significant flexibility in the way that the blade loading can be represented. The predictions of two models for the local blade aerodynamics are compared for all three of the HART II flight cases. The first model is a simple lifting-line model and the second is a somewhat more sophisticated lifting-chord model based on unsteady thin aerofoil theory. A marked improvement in accuracy of the predicted high-frequency airloads and acoustic signature of the HART II rotor is obtained when the lifting-chord model for the blade aerodynamics is used instead of the lifting-line type approach. Errors in the amplitude and phase of the loading peaks are reduced and the quality of the prediction is affected to a lesser extent by the computational resolution of the wake. Predictions of the acoustic signature of the rotor are similarly affected, with the lifting-chord model at the highest resolution producing the best representation of the distribution of sound pressure on the ground plane below the rotor.

Item type: Conference or Workshop Item (Paper)
ID code: 27437
Keywords: hart II rotor, vorticity transport model, high-frequency airloads, blade-vortex interactions, lifting-chord model, acoustic signature, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Mechanical Engineering, Aerospace Engineering, Computational Mechanics, Modelling and Simulation
Subjects: Technology > Mechanical engineering and machinery
Technology > Motor vehicles. Aeronautics. Astronautics
Department: Faculty of Engineering > Mechanical and Aerospace Engineering
Depositing user: Ms Katrina May
Date Deposited: 13 Sep 2010 14:20
Last modified: 24 Jul 2015 06:52
URI: http://strathprints.strath.ac.uk/id/eprint/27437

Actions (login required)

View Item View Item