Assessment of the thermal environment in an aircraft cabin

    Research output: Chapter in Book/Report/Conference proceedingArticle in proceedingsResearchpeer-review


    A full-scale section of a flight cabin with 21 seats was used to study the thermal environment in aircraft under laboratory conditions. Fourteen heated cylinders and two thermal manikins were used to simulate the heat load, the buoyancy flow and the flow obstruction from passengers in the cabin. Mean air velocities were measured in the range 0.105 ¿ 0.658 m/s. The measured air temperature differed by -0.6°C to + 2.1°C from the set point temperature. The whole-body equivalent temperature was 1.5-2°C lower in the outer seats than in the middle seat. The largest asymmetry in the segmental equivalent temperature, up to 5.8°C, was identified in the outer seats. The results reveal that in an aircraft cabin, passengers in the outer seats may be exposed to thermal asymmetry and draught and may not find the thermal environment acceptable if the ventilation air is not properly supplied.
    Original languageEnglish
    Title of host publicationProcedings of Roomvent 2004
    VolumeCD Rom
    PublisherUniversity of Coimbra
    Publication date2004
    Publication statusPublished - 2004
    Event9th International Conference on Air Distribution in Rooms - University of Coimbra, Coimbra, Portugal
    Duration: 5 Sept 20048 Sept 2004
    Conference number: 9


    Conference9th International Conference on Air Distribution in Rooms
    LocationUniversity of Coimbra


    Dive into the research topics of 'Assessment of the thermal environment in an aircraft cabin'. Together they form a unique fingerprint.

    Cite this