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Supersonic Jets Issued into Confined Spaces

Text Box: Shock angles when tube located at -8.1 mm downstream of the nozzle     £    Short tube Long tube     Long tube                                                                       

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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