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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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