Need ASAP. Thank you! 1. The angle of attack (?) of a wing-body combination varies with its lift coefficient ?? as follows: a
Need ASAP. Thank you! 1. The angle of attack (?) of a wing-body combination varies with its lift coefficient ?? as follows: a
Advanced Engineering Mathematics
10th Edition
ISBN:9780470458365
Author:Erwin Kreyszig
Publisher:Erwin Kreyszig
Chapter2: Second-order Linear Odes
Section: Chapter Questions
Problem 1RQ
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Need ASAP. Thank you!
1. The angle of attack (?) of a wing-body combination varies with its lift
coefficient ?? as follows:
a | 2.5 | 5.0 | 7.5 |
CL | 0.17 | 0.13 | 0.44 |
a) Use central difference (CD) of the Taylor Series to calculate ???/??.
b) Combine Taylor Series Expansions (BWD and FWD) with Cramer’s Rule to
determine the 1st derivative (??/???).
c) Calculate ??/???
from (a) and compare the result with that from (b)
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