Investigation of thermal comfort in aircraft cabin by means of Comfort zones model
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F11%3APU96704" target="_blank" >RIV/00216305:26210/11:PU96704 - isvavai.cz</a>
Výsledek na webu
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DOI - Digital Object Identifier
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Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Investigation of thermal comfort in aircraft cabin by means of Comfort zones model
Popis výsledku v původním jazyce
The thermal comfort of passengers in the aircraft first class suite using comfort zones model (according to standard ISO 14505-2) was performed and the CFD method was employed. Several different positions of personal inlets and flow rates were tested. The study was performed in the section of the Airbus A380 aircraft lining with 4 seats occupied by passive manikins. Manikins' boundary conditions were equal to the ISO 14505 summer comfort zones diagram. The study shows specifics of implementation of comfort zones model in CFD and predicts which combination of inlets are feasible for personalised ventilation in aircraft cabin. The main goal of the study was reach the overall and local thermal comfort in combination with personalised ventilation. All models and simulations were performed under commercial CFD code Star-CCM+.
Název v anglickém jazyce
Investigation of thermal comfort in aircraft cabin by means of Comfort zones model
Popis výsledku anglicky
The thermal comfort of passengers in the aircraft first class suite using comfort zones model (according to standard ISO 14505-2) was performed and the CFD method was employed. Several different positions of personal inlets and flow rates were tested. The study was performed in the section of the Airbus A380 aircraft lining with 4 seats occupied by passive manikins. Manikins' boundary conditions were equal to the ISO 14505 summer comfort zones diagram. The study shows specifics of implementation of comfort zones model in CFD and predicts which combination of inlets are feasible for personalised ventilation in aircraft cabin. The main goal of the study was reach the overall and local thermal comfort in combination with personalised ventilation. All models and simulations were performed under commercial CFD code Star-CCM+.
Klasifikace
Druh
O - Ostatní výsledky
CEP obor
BJ - Termodynamika
OECD FORD obor
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Návaznosti výsledku
Projekt
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Návaznosti
S - Specificky vyzkum na vysokych skolach
Ostatní
Rok uplatnění
2011
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů