In supersonic wind tunnel testing, if different gases areused, dynamic similarity requires that the model and prototypehave the same Mach number and the same( a ) Euler number, ( b ) speed of sound, ( c ) stagnation enthalpy,( d ) Froude number, ( e ) specific-heat ratio

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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In supersonic wind tunnel testing, if different gases are
used, dynamic similarity requires that the model and prototype
have the same Mach number and the same
( a ) Euler number, ( b ) speed of sound, ( c ) stagnation enthalpy,
( d ) Froude number, ( e ) specific-heat ratio

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