An airplane, of overall length 55 ft, is designed to fl y at680 m/s at 8000-m standard altitude. A one-thirtieth-scalemodel is to be tested in a pressurized helium wind tunnel at20 ° C. What is the appropriate tunnel pressure in atm? Evenat this (high) pressure, exact dynamic similarity is notachieved. Why?
An airplane, of overall length 55 ft, is designed to fl y at680 m/s at 8000-m standard altitude. A one-thirtieth-scalemodel is to be tested in a pressurized helium wind tunnel at20 ° C. What is the appropriate tunnel pressure in atm? Evenat this (high) pressure, exact dynamic similarity is notachieved. Why?
College Physics
1st Edition
ISBN:9781938168000
Author:Paul Peter Urone, Roger Hinrichs
Publisher:Paul Peter Urone, Roger Hinrichs
Chapter13: Temperature, Kinetic Theory, And The Gas Laws
Section: Chapter Questions
Problem 38PE: (a) In the deep space between galaxies, me density of atoms is as low as 106atoms/m3, and me...
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An airplane, of overall length 55 ft, is designed to fl y at
680 m/s at 8000-m standard altitude. A one-thirtieth-scale
model is to be tested in a pressurized helium wind tunnel at
20 ° C. What is the appropriate tunnel pressure in atm? Even
at this (high) pressure, exact dynamic similarity is not
achieved. Why?
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