Question

3 PL 23.5 Laminar slit flow with a moving wall (plane Couette flow). Extend Problem 23.4 by allow- ing the wall at x B to m

12 Lipuli on Draw carefully labeled sketches of these functions. Answers: (a) „(v) = (*7*2)=- (b) v.Cx) = (*72)P [1-(0))+ (1


2B.4 Laminar flow in a narrow slit (see Fig. 2B.4). (a) An incompressible Newtonian fluid is in laminar flow in a narrow slit
0 0
Add a comment Improve this question Transcribed image text
Answer #1

S ; Given that, 1. The fluid flows in Z-direction. whese, Velocity = function of x -> VZ = vz6327 Here: - z momentum in PositThen the Pressure in Z-directions P=P(z) Given diagram Y =WA -- 90 - yao ct øzzle ------ ZEL L T Direction of gravity THAL 50L Now -> gzz = 8zz +zz + luz vz = P(z) +evz? -> (760) - PC) + Pg 1) - dotz o - PL07-2960 - [PCD=691] - dpsz -. As, we know hei. vz = 2UL :V = (R: )? [-(41)+ Y2 (14) As, Taza-M (duz (de); we get - Txz = -4 (- Po-PL x + y ) 2. Finally we get : Tzz = Po

Add a comment
Know the answer?
Add Answer to:
3 PL 23.5 Laminar slit flow with a moving wall ("plane Couette flow"). Extend Problem 23.4...
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for? Ask your own homework help question. Our experts will answer your question WITHIN MINUTES for Free.
Similar Homework Help Questions
  • 283 Laminar fow in a narrow slit (see Fig, 2B.3), Fluid in Fluid outFig. 2B.3 Flow...

    283 Laminar fow in a narrow slit (see Fig, 2B.3), Fluid in Fluid outFig. 2B.3 Flow through a slit, with B< W<<L a) A Newtonian fluid is in laminar flow in a narrow slit formed by two parallel walls a dis tance 2B apart. It is understood that B <W, so that "edge effects" are unimportant. Make a differential momentum balance, and obtain the following expressions for the momentum-flux and velocity distributions ", " (부). (2B.3-1) (P )B (2B.3-2) In...

  • 12. Consider steady, incompressible, parallel, laminar flow of a film of oil falling slowly down an...

    12. Consider steady, incompressible, parallel, laminar flow of a film of oil falling slowly down an infinite vertical wall as shown in the figure(Fig. P12a). The oil film thickness is h, and gravity acts in the negative z-direction (downward in the figure) There is no applied (forced) pressure driving the flow the oil falls by gravity alone. (1) Calculate the velocity field in the oi film and sketch the normalized velocity profile. And generate an expression for the volumetric flow...

  • Please attempt the FULL QUESTION Question 4 For pressure-driven laminar flow between two horizontal infinite parallel...

    Please attempt the FULL QUESTION Question 4 For pressure-driven laminar flow between two horizontal infinite parallel plates separated by a distance 2h, the velocity components are: v = 0 where U is the centreline velocity and the x-axis is located at the centreline. Assume steady, fully developed and incompressible laminar flow. For the problem above, obtain the final form of the energy equation after applying the given assumptions. (10 marks) b) Identify the fluid temperature distribution T(y), for a constant...

  • An important problem in chemical engineering separation equipment involves thin liquid films flow...

    An important problem in chemical engineering separation equipment involves thin liquid films flowing down vertical walls due to gravity, as shown in this figure yV A. Assume that the wall is long and wide compared to the film thickness, with steady flow that is laminar and fully developed: u= v=0 and w w(x). Using a force balance on a rectangular differential element, derive an expression relating g, p, and τΧΖ . Use τΧΖ-n(-_ +--) for a Newtonian fluid to convert...

  • Fr the falling fm . Lerive anl vcloci Pey o 42) assumin 5 usinte equatienmtion (6.5-3), niam it...

    fr the falling fm . Lerive anl vcloci Pey o 42) assumin 5 usinte equatienmtion (6.5-3), niam ity, average velocity, or force on solid surfaces. tion appear, and In the integrations mentioned above, several constants of integration a the velocit stress at the boundaries of the system. The most commonly used boundae are as follows: using "boundary conditions"-that is, statements about a. At solid-fluid interfaces the fluid velocity equals the velocity with which surface is moving: this statement is applied...

  • BIG UPVOTE FOR RIGHT ANSWER Viscous fluid flow 2nd edition Frank White I need answer of...

    BIG UPVOTE FOR RIGHT ANSWER Viscous fluid flow 2nd edition Frank White I need answer of 2.17 I have attached 2.14 question and solution for reference. 2.17 As an extension of Prob. 2-14, consider the heat-transfer aspect by assuming a uniform entrance profile T = To and an exit profile approximated by T(r) = T0(1.5 + 0.5r2/ri). For flow with constant (p, F, cp, k) and negligible kinetic- and potential-energy changes, use the integral relations to compute the total heat...

  • just now i sent this questions. this is the answer given. however the answer i afraid...

    just now i sent this questions. this is the answer given. however the answer i afraid that he used formula that is not for constant surface temperature and noncircular formula. this is the formula foe the noncircular tube. because the question ask about triangle. my problem is, i cannot answer question 1(b) that ask the heat transfer coefficient, h. please help me. thank you. this pic is a note on constant surface temperature. page 482 ref: HEAT AND MASS TRANSFER:...

ADVERTISEMENT
Free Homework Help App
Download From Google Play
Scan Your Homework
to Get Instant Free Answers
Need Online Homework Help?
Ask a Question
Get Answers For Free
Most questions answered within 3 hours.
ADVERTISEMENT
ADVERTISEMENT
ADVERTISEMENT