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Ok.. having problems calculating IAP ratio... sortof... I know that IAP ratio is P_0 / p where P_0 is 29.92126 and p is pressure at altitude. In a spreadsheet the formula I'm using to calculate pressure at altitude is
p = P_0 * POWER((1-0.0000068755856 * altitude),5.2558797).
So, in the sim I slew to 35000 feet and the ambient pressure is 7.0599220670618816. My spreadsheet calculates it at 7.040620526 which is off a tad, and I'm really uncertain as to why that would be.
Any thoughts? Suggestions?
p = P_0 * POWER((1-0.0000068755856 * altitude),5.2558797).
So, in the sim I slew to 35000 feet and the ambient pressure is 7.0599220670618816. My spreadsheet calculates it at 7.040620526 which is off a tad, and I'm really uncertain as to why that would be.
Any thoughts? Suggestions?


