8.1. An airplane wing of 3 m chord length moves through still air at 15°C and 101.3 kPa at a speed of 320 km/h. A !: 20 scale model of this wing is placed in a wind tunnel, and dynamic similarity between model and prototype is desired. (a) What velocity is necessary in a tunnel where the air has the same pressure and temperature as that in flight? (b) What velocity is necessary in a variable-density wind tunnel where absolute pressure is 1 400 kPa and temperature is 15°C? (c) At what speed must the model move through water (15°C) for dynamic similarity?

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
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Chapter5: Analysis Of Convection Heat Transfer
Section: Chapter Questions
Problem 5.70P
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8.1. An airplane wing of 3 m chord length moves through still air at 15°C and 101.3 kPa at a
speed of 320 km/h. A !:20 scale model of this wing is placed in a wind tunnel, and dynamic
similarity between model and prototype is desired. (a) What velocity is necessary in a tunnel
where the air has the same pressure and temperature as that in flight? (b) What velocity is
necessary in a variable-density wind tunnel where absolute pressure is 1 400 kPa and temperature
is 15°C? (c) At what speed must the model move through water (15°C) for dynamic similarity?
Transcribed Image Text:8.1. An airplane wing of 3 m chord length moves through still air at 15°C and 101.3 kPa at a speed of 320 km/h. A !:20 scale model of this wing is placed in a wind tunnel, and dynamic similarity between model and prototype is desired. (a) What velocity is necessary in a tunnel where the air has the same pressure and temperature as that in flight? (b) What velocity is necessary in a variable-density wind tunnel where absolute pressure is 1 400 kPa and temperature is 15°C? (c) At what speed must the model move through water (15°C) for dynamic similarity?
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