Engineering Mechanics: Statics
8th Edition
ISBN: 9781118807330
Author: James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher: WILEY
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Chapter 6.3, Problem 2P
The 50-kg block rests on the horizontal surface, and a force
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Just do Questions 7, 9, 11. Here are notes attached for reference. I prefer handwritten solutions. ONLY UPLOAD A SOLUTION IF YOU ARE SURE ABOUT THE ANSWER PLEASE.
This is a tilt and rotation question. Here are notes attached for reference. I prefer handwritten solutions. ONLY UPLOAD A SOLUTION IF YOU ARE SURE ABOUT THE ANSWER PLEASE. I prefer handwritten solutions.
A turbine blade made of a metal alloy (k = 17 W/m-K) has a
length of 5.3 cm, a perimeter of 11 cm, and a cross-sectional
area of 5.13 cm². The turbine blade is exposed to hot gas
from the combustion chamber at 1133°C with a convection
heat transfer coefficient of 538 W/m²K. The base of the
turbine blade maintains a constant temperature of 450°C
and the tip is adiabatic.
NOTE: This is a multi-part question. Once an answer is
submitted, you will be unable to return to this part.
Hot gas
h=538 W/m²K
TL
E=
Turbine blade
k = 17 W/m-K
p=11 cm, L=5.3 cm
A = 5.13cm²
T=450°C
Determine the temperature at the tip of the turbine blade.
The temperature at the tip of the turbine blade is
°C.
Chapter 6 Solutions
Engineering Mechanics: Statics
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