A two-dimensional airfoil (object 1) is subject to air flow of upstream velocity 24 m/s. The upstream air pressure and temperature are 0.6 atm and 280 K, respectively. The characteristic length of object 1 is 29 mm and its surface temperature is uniform at 320 K. Now, a geometrically similar airfoil (object 2) with a different characteristic length 212 mm is placed in water flow. The upstream water temperature is 300 K and the surface temperature of object 2 is uniformly at 310 K. What is the upstream water velocity in m/s for object 2 such that the boundary layer analogy exists between the two cases? Note that liquid water properties can be approximated as those for a saturated liquid at the same temperature. Object 1 Ts1 Air Too1 V₁ L₁ Water Too2 V₂ Object 2 L₂ Ts2

A two-dimensional airfoil (object 1) is subject to air flow of upstream velocity 24 m/s. The upstream air pressure and temperature are 0.6 atm and 280 K, respectively. The characteristic length of object 1 is 29 mm and its surface temperature is uniform at 320 K. Now, a geometrically similar airfoil (object 2) with a different characteristic length 212 mm is placed in water flow. The upstream water temperature is 300 K and the surface temperature of object 2 is uniformly at 310 K. What is the upstream water velocity in m/s for object 2 such that the boundary layer analogy exists between the two cases? Note that liquid water properties can be approximated as those for a saturated liquid at the same temperature. Object 1 Ts1 Air Too1 V₁ L₁ Water Too2 V₂ Object 2 L₂ Ts2

Name: A two-dimensional airfoil (object 1) is subject to air flow of upstre
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Description: A two-dimensional airfoil (object 1) is subject to air flow of upstream velocity 24m/s. The upstream air pressure and temperature are 0.6 atm and 280 K,respectively. The characteristic length of object 1 is 29 mm and its surfacetemperature is unifor

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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