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Lastly a section is presented that describes the module integration into a riding simulator and a discussion of the preliminary results.
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Figure 2 Model of the open ended galvanic coupled quarter-wave coaxial resonator with connected flush to a waveguide pipe section is presented on the left.
The pitch/yaw apparatus designed for the measurement of the moment derivative due to an aircraft or missile model angular oscillatory motion in a wind tunnel test section is presented.
The result section is presented in a way that claims an ability of complementing qualitative with quantitative findings which could be questioned.
The final score from each section is presented as a percentage of the maximum detrimental impact with a higher percentage, indicating greater symptom impact or worse QoL.
The cross section is presented as a function of the jet transverse momentum in the range 18 < p(T) < 200 GeV for several rapidity intervals.
This section is presented in a narrative form.
The data in each section is presented in an un-tidied format to preserve the integrity of the women's account.
This section is presented through four subsections.
Local distribution of friction factor ratio and Nusselt number across a cross-section is presented.
In addition, the spatial distribution of vascular bundles, pith and fibers over a plant cross section was presented.
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Since I tried Ludwig back in 2017, I have been constantly using it in both editing and translation. Ever since, I suggest it to my translators at ProSciEditing.

Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com