Assume that, at a point on the wing of the Concorde supersonic transport, the air temperature is -1.5°C and the pressure is 1.66 x 10^4 N/m 2. Calculate the densit (in kg/m^3) at this point. Note: Specific Heat of Air in Metric Unit, R = 287 J/kg*K​

find out the value of b

step-by-step explanation:

b) 1/3 * 1/5

step-by-step explanation:

each smallest part is 1/15 since the written one is 1/5 and it's divided by 3 equal parts. (1/5 )/3 = 1/15 = 1/3 * 1/5

0,0

step-by-step explanation:

step-by-step explanation:

*calories burned = (weight)(calorie factor)*

calories burned = 180 (0.65)

calories burned = 117

the calories he used up is 117, which is 65% of his weight.