Tb = 250°C8mm120mmK= 300 Wmkh=160W/m²KTx = 32°CMA2 mmfin = ?-L=50mmdetermine the temperature distributionand wing efficiency throughout the wingtaking into account the adiabatic boundythe acceptance ofone-dimensional heat transfer in acontinuous regime for the thin-tip airfoilwith the shape shown in figure

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

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

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Question

Tb = 250°C
8mm
120mm
K= 300 W
mk
h=160W/m²K
Tx = 32°C
MA
2 mm
fin = ?
-L=50mm
determine the temperature distribution
and wing efficiency throughout the wing
taking into account the adiabatic boundy
the acceptance of
one-dimensional heat transfer in a
continuous regime for the thin-tip airfoil
with the shape shown in figure

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