Question

TRUE FALSE of this ctew factors Fia and Fas for the following. Surface 1 is the circular bottom ine and surface 2 is every other surface inside this cylindrical dome. b. (10 points) a and Fas for the follow L 1.0m Consider the plate below. Does the flow down this plate transition to turbulence, and if so at what x value? c. (10 points) Properties for air: k 0.02953 Wim-K 2.097 x 105 m2/s Pre 0.7154 U-25 m/s 0.9994 kg/m3 Cp-1008 J/kg-K 0.5 m (5 points) The Prandtl number can be considered a ratio of momentum diffusivity thermal diffusivity. If the Prandtl number is greater than 1, which is thicker at given location, the thermal boundary layer or the hydrodynamic boundary layer CIRCLE ONE Thermal Hydrodynamic
0 0
Add a comment Improve this question Transcribed image text
Know the answer?
Add Answer to:
TRUE FALSE of this ctew factors Fia and Fas for the following. Surface 1 is the...
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
  • (2 pts) Heat is transferred from a hot fluid (temperature T1 and heat transfer coefficient h2)...

    (2 pts) Heat is transferred from a hot fluid (temperature T1 and heat transfer coefficient h2) through a plane wall of thickness 8, surface area A and the thermal conductivity k. The thermal resistance for the set up is + (a) AC ) (b) A (i + + ) (c) 2 (na + + n2) (d) A (na + b +h2) (2 pts) An increase in convective heat transfer coefficient over a fin will (a) increase effectiveness (b) decrease effectiveness...

  • 3. Consider the following fluids at a film temperature of 300 K in parallel flow over...

    3. Consider the following fluids at a film temperature of 300 K in parallel flow over a flat plate with velocity of 1 m/s: atmospheric air and mercury. a. For each fluid, estimate the velocity and thermal boundary layer thicknesses at a distance of 40 mm from the leading edge. (4 pts for each boundary layer thickness determination. Total 16 pts) At what distance from the leading edge, do the boundary layers of air and mercury transition to turbulence? (5...

  • Exercise 2 Air at 20 °C and 1 atm flows over a flat plate at 50...

    Exercise 2 Air at 20 °C and 1 atm flows over a flat plate at 50 m/s. The plate is 300 cm long and is maintained at 60C. The width of the plate is 2 m. The critical Rec = 5 x 105 The properties are Conductivity k = 0.0263 W/mK, kinematic viscosity nu = v = 15.89 x 10-6 m²/s, Prandtl number is Pr=0.707 Density rho = p = 1.128 kg/m3 1. Determine the critical length Xc 2. Determine...

  • Air at T=25°C and pressure P=1 bar flows over a square plate with a velocity V=1...

    Air at T=25°C and pressure P=1 bar flows over a square plate with a velocity V=1 m/s. This plate has a length L= 1 m and it is heated over its entire length; the plate temperature is constant Tp=100°C. The following data are given. For air: dynamic viscosity: mu = 1.9*10–5 kg/(m.s); density: rho = 1.05 kg/m3; conductivity k = 0.03 W/(m K); Specific heat Cp = 1.007 kJ/(kg K); Prandtl number Pr = 0.7 For laminar flow over a...

  • Question 1 [40 Points] Liquid mercury at 300 K flows over a flat surface at a...

    Question 1 [40 Points] Liquid mercury at 300 K flows over a flat surface at a free stream velocity 0.15 m/s. The flat plate is smooth with a width of 0.25 m and length 0.5 m and is kept at a uniform temperature of 400 K. The flow is parallel to the longer dimension of the plate. Find out: 1. MINIMUM LOCAL convective heat flux, q min and its location (60%) 2. Total convective heat transfer rate, q (40%) Use...

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