For the shown continuously circular (i.e. not parabolic) arc airfoil with sharp corners of each 8 = 5º, at 0° angle of attack with M∞ = 3 and assuming steady, two-dimensional flow, calculate the: a) pressure coefficient distribution; b) lift coefficient; c) drag coefficient. Moo S ********** 8

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
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must use thin airfoil theory

Need only handwritten solution only (not typed one).

For the shown continuously circular (i.e. not parabolic) arc airfoil with sharp corners of each
8 = 5°, at 0° angle of attack with Mo = 3 and assuming steady, two-dimensional flow,
calculate the:
a) pressure coefficient distribution;
b) lift coefficient;
c) drag coefficient.
Moo
8
*********
8
Transcribed Image Text:For the shown continuously circular (i.e. not parabolic) arc airfoil with sharp corners of each 8 = 5°, at 0° angle of attack with Mo = 3 and assuming steady, two-dimensional flow, calculate the: a) pressure coefficient distribution; b) lift coefficient; c) drag coefficient. Moo 8 ********* 8
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