2015
DOI: 10.1016/j.buildenv.2015.06.030
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Global airflow field distribution in a cabin mock-up measured via large-scale 2D-PIV

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Cited by 58 publications
(55 citation statements)
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References 33 publications
(37 reference statements)
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“…The body geometry is obtained by scanning a thermal manikin, which neglects the clothes and hair. The distance from the head top to the ceiling is 24 cm, which is obtained by the model measurement of an airplane cabin with manikin directly, and is consistent with the size of related researches (Li et al 2015;Zhang et al 2009). It can be considered that this distance represents a typical environment condition of body thermal plume in cabin.…”
Section: Calculation Domain and Boundary Conditionsmentioning
confidence: 98%
“…The body geometry is obtained by scanning a thermal manikin, which neglects the clothes and hair. The distance from the head top to the ceiling is 24 cm, which is obtained by the model measurement of an airplane cabin with manikin directly, and is consistent with the size of related researches (Li et al 2015;Zhang et al 2009). It can be considered that this distance represents a typical environment condition of body thermal plume in cabin.…”
Section: Calculation Domain and Boundary Conditionsmentioning
confidence: 98%
“…DEHS droplets are very promising particles for PIV measurements for their good tracking ability and high stability [16]. Moreover, compared with the theatrical fog machines used in previous studies [16,26], although the Laskin aerosol generator with a high generation rate to maintain the seeding concentration in the cabin is expensive, its generation rate is controllable and continuous, which are necessary for acquiring accurate instantaneous velocity fields for a long time series.…”
Section: Piv Measurement Setupmentioning
confidence: 99%
“…Under cooling conditions, the air supply temperature remained at 19.0 • C (±0.5 • C), and the averaged air temperature in the cabin was increased to 22.7 • C due to the heated manikins, and the detailed thermal boundary condition could be found in Ref. [26]. Between two operational conditions, there were at least 90 min to ensure the stable condition was reached.…”
Section: Aircraft Cabin Mock-upmentioning
confidence: 99%
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