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    Altitude Change Calculation

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    psn_kylm
    The document calculates changes in air pressure based on an increase in altitude using CIBSE Equation C1.12. It shows that at sea level the pressure is 101.325 kPa and density is 1.200 kg/cum. For an altitude increase of 1,000 meters, the pressure decreases to 90.211 kPa, representing a pressure change of -11.114 kPa.

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    Altitude Change Calculation

    Uploaded by

    psn_kylm
    28 views1 page
    The document calculates changes in air pressure based on an increase in altitude using CIBSE Equation C1.12. It shows that at sea level the pressure is 101.325 kPa and density is 1.200 kg/cum. For an altitude increase of 1,000 meters, the pressure decreases to 90.211 kPa, representing a pressure change of -11.114 kPa.

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    The document calculates changes in air pressure based on an increase in altitude using CIBSE Equation C1.12. It shows that at sea level the pressure is 101.325 kPa and density is 1.200 kg/cum. For an altitude increase of 1,000 meters, the pressure decreases to 90.211 kPa, representing a pressure change of -11.114 kPa.

    Copyright:

    © All Rights Reserved
    Download as XLS, PDF, TXT or read online from Scribd
    Download as xls, pdf, or txt
    28 views1 page

    Altitude Change Calculation

    Uploaded by

    psn_kylm
    The document calculates changes in air pressure based on an increase in altitude using CIBSE Equation C1.12. It shows that at sea level the pressure is 101.325 kPa and density is 1.200 kg/cum. For an altitude increase of 1,000 meters, the pressure decreases to 90.211 kPa, representing a pressure change of -11.114 kPa.

    Copyright:

    © All Rights Reserved
    Download as XLS, PDF, TXT or read online from Scribd
    Download as xls, pdf, or txt
    of 1

    04/24/2020 472092412.

    xls 10:09:41

    Calculation based on CIBSE Equation C1.12


    Pressure at Sea level 101.325 (kPa)
    Density at Sea level 1.200 (kg/cum)
    Altitude increase 1,000 (m)
    Pressure at new altitude 90.211 (kPa)
    Pressure change -11.114 (kPa)

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