Th=250°C8mm-120mm-L= 50mmK= 300 WMKh=160W/m²KT= 32°CTimmn fin = ?determine the temperature distributionand wing efficiency throughout the wingboundytaking into account the adiabaticat the wing tips under the acceptance ofone-dimensional heat transfer in acontinuous regime for the thin-tip airfoilfigurewith the shape shown in

Answered: Image /qna-images/answer/6f036773-14b5-498a-bb46-97ea81c26635.jpg

determine the temperature distribution and wing efficiency throughout the wing taking into account the adiabatic bourdy acceptance of the one-dimensional heat transfer in a continuous regime for the thin-tip airfoil worth the shape shown in figure

determine the temperature distribution and wing efficiency throughout the wing taking into account the adiabatic bourdy acceptance of the one-dimensional heat transfer in a continuous regime for the thin-tip airfoil worth the shape shown in figure

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter5: Analysis Of Convection Heat Transfer

Section: Chapter Questions

Problem 5.25P

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Question

Th=250°C
8mm
-120mm
-L= 50mm
K= 300 W
MK
h=160W/m²K
T= 32°C
Timm
n fin = ?
determine the temperature distribution
and wing efficiency throughout the wing
boundy
taking into account the adiabatic
at the wing tips under the acceptance of
one-dimensional heat transfer in a
continuous regime for the thin-tip airfoil
figure
with the shape shown in

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