Florida International University Department of Civil and...

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Florida International University Department of Civil and Environmental Engineering CWR 3201 Fluid Mechanics Fall 2018 Instructor: Arturo S. Leon, Ph.D., P.E., D.WRE TA: Thao Do, CEE Undergraduate Homework Assignment 3 Solutions Mechanics of Fluids (Fifth edition), by M.C. Potter, D.C. Wiggert and B.H. Ramadan. 1. 3.18 (same number in Fourth edition) a) cos = !! ! = !!! ! !!! ! ! ! !! ! = 0.832 = 33 .69 To calculate the normal: = 0 3 + 2 ! + ! = 0 3 ! + 2 ! = 0 : ! ! + ! ! = 1 Solving system of equations gives: = ! !" (2 3 ) Part b and c are the same steps except V is given as different equations 2. 3.19 (same number in Fourth edition) a) × = 0 + 2 + × + = 0 + 2 = 0 OR !"! !!! = : + 2 = 2 + 2 = + Plug in streamline point values to solve for coefficient C: 2 1 23 = 2 + = 0.8028 Equation of the streamline: 2 + 2 = + 0 .8028 Part b and c are the same steps but different equations to integrate 3. 3.28 a. Along the center of the pipe r=0 cm: = 2 1 0 1 ! ! !" = 2 = ! = = 2 1 0 1 10 ! ! !" = 0 .2 ! = 0

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Page 1: Florida International University Department of Civil and ...web.eng.fiu.edu/...Mechanics/.../HW3_2018_SOLUTION.pdf · Florida International University Department of Civil and Environmental

Florida International University Department of Civil and Environmental Engineering

CWR 3201 Fluid Mechanics

Fall 2018 Instructor: Arturo S. Leon, Ph.D., P.E., D.WRE

TA: Thao Do, CEE Undergraduate Homework Assignment 3 Solutions

Mechanics of Fluids (Fifth edition), by M.C. Potter, D.C. Wiggert and B.H. Ramadan.

1. 3.18 (same number in Fourth edition)

a) cos𝛼 = !∙!!= !!! !!!! ∙ !

!!!!!= 0.832

𝛼 = 33.69 𝑑𝑒𝑔 To calculate the normal: 𝑉 ∙ 𝑛 = 0

3𝚤 + 2𝚥 ∙ 𝑛!𝚤 + 𝑛!𝚥 = 0 3𝑛! + 2𝑛! = 0

𝑈𝑛𝑖𝑡 𝑣𝑒𝑐𝑡𝑜𝑟: 𝑛!! + 𝑛!! = 1

Solving system of equations gives: 𝑛 = !!"(2𝚤 − 3𝚥)

Part b and c are the same steps except V is given as different equations 2. 3.19 (same number in Fourth edition) a) 𝑉 × 𝑑𝑟 = 0

𝑥 + 2 𝚤 + 𝑥𝑡𝚥 × 𝑑𝑥𝚤 + 𝑑𝑦𝚥 = 0 𝑥 + 2 𝑑𝑦 − 𝑥𝑡𝑑𝑥 = 0 OR 𝑡 !"!

!!!= 𝑑𝑦

𝐼𝑛𝑡𝑒𝑔𝑟𝑎𝑡𝑒: 𝑡𝑥𝑑𝑥𝑥 + 2 = 𝑑𝑦

𝑡 𝑥 − 2𝑙𝑛 𝑥 + 2 = 𝑦 + 𝐶 Plug in streamline point values to solve for coefficient C: 2 1− 2𝑙𝑛3 = −2+ 𝐶

𝐶 = 0.8028 Equation of the streamline: 𝑡 𝑥 − 2𝑙𝑛 𝑥 + 2 = 𝑦 + 0.8028 Part b and c are the same steps but different equations to integrate

3. 3.28

a. Alongthecenterofthepiper=0cm:

𝑢 = 2 1 − 0 1 − 𝑒!!!" = 2

𝑚𝑠𝑤ℎ𝑒𝑛 𝑡 = ∞

𝑎! =𝜕𝑢𝜕𝑡

= 2 1 − 0110

𝑒!!!" = 0.2

𝑚𝑠!𝑎𝑡 𝑡 = 0

Page 2: Florida International University Department of Civil and ...web.eng.fiu.edu/...Mechanics/.../HW3_2018_SOLUTION.pdf · Florida International University Department of Civil and Environmental

b. Atr=0.5cm:𝑢 = 2 1 − !.!!

!!1 − 𝑒!

!!" = 1.875!

!𝑤ℎ𝑒𝑛 𝑡 = ∞

𝑎! =𝜕𝑢𝜕𝑡

= 2 1 −0.5!

2!110

𝑒!!!" = 0.1875

𝑚𝑠!𝑎𝑡 𝑡 = 0

c. Alongthewall,r=2cm(entiretyofthetube):𝑢 = 2 1 − !!

!!1 − 𝑒!

!!" =

0!!𝑤ℎ𝑒𝑛 𝑡 = 𝑎𝑙𝑙 𝑡𝑖𝑚𝑒

𝑎! =𝜕𝑢𝜕𝑡

= 2 1 −2!

2!110

𝑒!!!" = 0

𝑚𝑠!𝑎𝑡 𝑡 = 𝑎𝑙𝑙 𝑡𝑖𝑚𝑒

4. 3.35

a. 𝐴 = 2 20𝑘×12𝚤 + 20𝑘× 20𝑘×4.5𝚤 = 480 𝚥 − 1800𝚤 𝑓𝑡/𝑠!b. 𝐴 = 2 20𝑘×−60𝑐𝑜𝑠30𝚥 + 20𝑘× 20𝑘×4.5𝚤 = 278𝚤 𝑓𝑡/𝑠!

5. 3.45

ReynoldsNumber:𝑅𝑒 = !"!=

(!!! )(!.!"# !)

(!.!!!!"!!)= 38961Turbulent