Answer:
True
Explanation:
An aircraft is subject to 3 primary rotations
1) About longitudinal axis known as rolling
2) About lateral axis known as known as pitching
3) About the vertical axis known as yawing
The rolling of the aircraft induces torsion in the body of the aircraft thus the fuselage structure should be capable of carrying torsion
Answer:
Para x=0:
Para x=30 cm:
Explanation
Podemos utilizar la ley de Fourier par determinar el flujo de calor:
(1)
Por lo tanto debemos encontrar la derivada de T(x) con respecto a x primero.
Usando la ley de potencia para la derivda, tenemos:
![\frac{dT(x)}{dx}=300x-30](https://tex.z-dn.net/?f=%5Cfrac%7BdT%28x%29%7D%7Bdx%7D%3D300x-30)
Remplezando esta derivada en (1):
Para x=0:
![\phi=0.04(30)](https://tex.z-dn.net/?f=%5Cphi%3D0.04%2830%29)
Para x=30 cm:
![\phi=-0.04(300*0.3-30)](https://tex.z-dn.net/?f=%5Cphi%3D-0.04%28300%2A0.3-30%29)
Espero que te haya ayudado!
Answer:
See explaination
Explanation:
Please kindly check attachment for the step by step solution of the given problem.