4.6 The NACA 4412 airfoil has a mean camber line given by for 0 <=<0.4 0.25 0240-()] 0.8 for 0.4 <= 01 Using thin airfoil theory, calculate (a) aL-0 (b) c when a = 3°
4.6 The NACA 4412 airfoil has a mean camber line given by for 0 <=<0.4 0.25 0240-()] 0.8 for 0.4 <= 01 Using thin airfoil theory, calculate (a) aL-0 (b) c when a = 3°
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
For the airfoil given, calculate cm,c/4 and xcp/c when α = 3◦.
![4.6 The NACA 4412 airfoil has a mean camber line given by
for 0 <=<0.4
0.25
0240-()]
0.8
for 0.4 <=
01
Using thin airfoil theory, calculate
(a) aL-0 (b) c when a = 3°](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fbea8440a-fd89-4af5-a449-524c2104c300%2F889d8ad6-9c8e-4d26-a86a-4c3dac46e4ea%2F1bvndk.png&w=3840&q=75)
Transcribed Image Text:4.6 The NACA 4412 airfoil has a mean camber line given by
for 0 <=<0.4
0.25
0240-()]
0.8
for 0.4 <=
01
Using thin airfoil theory, calculate
(a) aL-0 (b) c when a = 3°
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