Question 1.

Calculate the temperature (in Kelvin) at an altitude of 9665 metres above sea level, assuming ISA atmosphere:

O -47.82

O 0.0065

O 350.82

O 12

O 225.18

Not answered Question 2.

Calculate the temperature (in Kelvin) at an altitude of 11471 metres above sea level, assuming ISA atmosphere:

0.0065

216.50

O 3

O 362.56

O-59.56

Not answered

SESSMEN sity

The Questions

Question 3.

Calculate the pressure (in Pascals) at an altitude of 5192 metres above sea level, assuming ISA atmosphere:

O -19

O 52611

O 90423

O 53

101325

[a2-alkarbi]

UFMFRU-15-1 DEWIS E-ASSE

Not answered The Questions

Question 4.

Calculate the air density (in kg per cubic metre) at an altitude of 12504 metres above sea level, assuming ISA atmosphere:

O 81.64

O 0.29

O 0.36

O 288.00

O-80.99

[a2-alk

UFMFRU-15-1 DEWIS E-AS

Not answered The Questions

Question 5.

An aircraft is flying at an altitude of 8364 m above sea level. Its airspeed with respect to the surrounding air is 137 m/s. Assuming ISA

conditions, calculate the dynamic pressure (in Pascals).

O 1965.1

O 288

-39.37

4716.52

O-928.7

OFMPRU-15-1 DEWIS E-ASSESSMEN

Not answered