Abstract

This paper addresses the influence of manufacturing variability of a helicopter rotor blade on its aeroelastic responses. An aeroelastic analysis using finite elements in spatial and temporal domains is used to compute the helicopter rotor frequencies, vibratory hub loads, power required and stability in forward flight. The novelty of the work lies in the application of advanced data-driven machine learning (ML) techniques, such as convolution neural networks (CNN), multi-layer perceptron (MLP), random forests, support vector machines and adaptive Gaussian process (GP) for capturing the nonlinear responses of these complex spatio-temporal models to develop an efficient physics-informed ML framework for stochastic rotor analysis. Thus, the work is of practical significance as (i) it accounts for manufacturing uncertainties, (ii) accurately quantifies their effects on nonlinear response of rotor blade and (iii) makes the computationally expensive simulations viable by the use of ML. A rigorous performance assessment of the aforementioned approaches is presented by demonstrating validation on the training dataset and prediction on the test dataset. The contribution of the study lies in the following findings: (i) The uncertainty in composite material and geometric properties can lead to significant variations in the rotor aeroelastic responses and thereby highlighting that the consideration of manufacturing variability in analyzing helicopter rotors is crucial for assessing their behaviour in real-life scenarios. (ii) Precisely, the substantial effect of uncertainty has been observed on the six vibratory hub loads and the damping with the highest impact on the yawing hub moment. Therefore, sufficient factor of safety should be considered in the design to alleviate the effects of perturbation in the simulation results. (iii) Although advanced ML techniques are harder to train, the optimal model configuration is capable of approximating the nonlinear response trends accurately. GP and CNN followed by MLP achieved satisfactory performance. Excellent accuracy achieved by the above ML techniques demonstrates their potential for application in the optimization of rotors under uncertainty.

Highlights

  • Helicopters experience high level of vibrations compared to other flight vehicles due to a significantly higher degree of aeroelastic interaction and rapidly rotating flexible blades [21]

  • The novelty of the work lies in the application of advanced data-driven machine learning (ML) techniques, such as convolution neural networks (CNN), multi-layer perceptron (MLP), random forests, support vector machines and adaptive Gaussian process (GP) for capturing the nonlinear responses of these complex spatio-temporal models to develop an efficient physics-informed ML framework for stochastic rotor analysis

  • The work is of practical significance as (i) it accounts for manufacturing uncertainties, (ii) accurately quantifies their effects on nonlinear response of rotor blade and (iii) makes the computationally expensive simulations viable by the use of ML

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Summary

Introduction

Helicopters experience high level of vibrations compared to other flight vehicles due to a significantly higher degree of aeroelastic interaction and rapidly rotating flexible blades [21]. Machine learning (for example, radial basis function neural network [29], recurrent neural network and multi-layer perceptron [30]) has been employed in solving inverse problems (for example, structural health monitoring, damage detection and model updating) for rotor blade applications previously, we observed that the literature is scarce when it comes to the application of ML for forward stochastic aeroelastic response analysis of rotors In this context, it is worth mentioning a recent work which has employed deep learning to emulate and extrapolate from the limited experimental responses of rotorcraft available as raw sensor (accelerometer) data and create a ’virtual sensor’ for better understanding of their vibration behaviour [36].

Aeroelastic analysis
Governing equations of motion
Finite element-spatial discretization
Normal mode transformation
Finite element-temporal discretization
Nt Z wiþ1
Aerodynamic loads
Rotor and hub loads
Coupled trim
General computational framework
Gaussian process modelling
Random forest
Support vector machine
Description of the parametric stochastic model
Adaptive Gaussian process
Convolution neural network: implementation details
Multi layer perceptron: implementation details
Random forest: implementation details
Support vector machine: implementation details
Results and discussion
Summary and conclusions
Full Text
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