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The results described in section 6 of this paper were obtained with one or the other triangulation method.
The data presented in this paper were obtained at the W. M. Keck Observatory, which is operated as a scientific partnership between the California Institute of Technology, the University of California and the National Aeronautics and Space Administration.
Experimental results presented in this paper were obtained by testing the engine with air as working fluid.
The principal shear modulus data presented in the paper were obtained by testing at a rotational speed of 1000 rpm.
The results presented in this paper were obtained during the AIV Assemblyy, Integration and Verification) pre-launch testing phase and during the post-launch commissioning phase.
The results in the paper were obtained on a laboratory scale actuator in test laboratories at the ALSTOM Power Technology Centre, Whetstone, UK.
The research results presented in this paper were obtained as part of the joint CSIRO-NASA Ageless Aerospace Vehicle (AAV) project.
We remark that all the SLM results presented in this paper were obtained using collocation points.
All weight percentages of carbon reported in this paper were obtained by elemental analysis.
The results reported in this paper were obtained based on the best possible combination of the parameters.
The results presented in this paper were obtained by implementing the genetic algorithm in the Matlab environment.
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