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( D 1 ) An aircraft's instruments measure an air temperature of 1 5 deg C and an air pressure of 8 3 kPa. What

(D1) An aircraft\'s instruments measure an air temperature of 15 deg C and an air pressure of 83 kPa. What is the density altitude for these conditions? (Use Equation 2.1 which is the Aero version of the Perfect Gas Law. Also, be sure to convert the temperature to absolute temperature and convert kPa to Pascals =N/m2. Then find the altitude in the SI standard atmosphere on page 566 that has this density.)

 

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