Question: An airplane, of overall length 55 ft, is designed to fly at 680 m/s at 8000-m standard altitude. A one-thirtieth-scale model is to be tested
An airplane, of overall length 55 ft, is designed to fly 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?
Step by Step Solution
3.42 Rating (168 Votes )
There are 3 Steps involved in it
For air at 8000m standard altitude Table A6 take 0525 kgm3 153E... View full answer
Get step-by-step solutions from verified subject matter experts
Document Format (1 attachment)
E-ME-FM (608).docx
120 KBs Word File
