Solution Manual For Fundamentals of Aerodynamics, 7th Edition by John Anderson.docx Chapter 1-19

Solution Manual For Fundamentals of Aerodynamics, 7th Edition John Anderson Chapter 1-19

CHAPTER 1 1.1

(a)

(b)



p 1.9  104   0.326 kg/m3 RT (287)(203)

T

p 1058   501 R R 1.23  103 (1716)





1.2

N    

TE LE

TE LE

 pu cos   u sin  dsu

 p cos    sin   ds

(1.7)

ds cos   dx ds cos   dy

Hence,

 pu  p  dx   LE  u    dy LE

N   

TE

N   

TE

TE

 p  p    p  p  dx    u    dy LE  u LE TE

Divide by q  S  q c(1)

  N 1 TE  p  p   p  p   1 TE       u  dx    u      dy qc c LE  q   q    c LE  q  q   cn 









1 c 1 TE c  c dx  cf  cfe dy p p u c 0 e c  LE n

This is Eq. (1.15). 1 © McGraw Hill LLC. All rights reserved. No reproduction or distribution without the prior written consent of McGraw Hill LLC.