0 votes
49 views
asked in Thermal by (215k points)
edited by

 For steady adiabatic flow of an ideal gas with constant specific heats through a nozzle or diffuser, show that:

        

 

 

 

Where To and T are the stagnation and static temperatures, respectively, k is the ratio of specific heats and M the Mach number.                      

Please log in or register to answer this question.

Welcome to Q&A discussion forum, where you can ask questions and receive answers from other members of the community.

10.4k questions

274 answers

26 comments

15.3k users

...