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Category > Engineering Posted 23 May 2017 My Price 6.00

what is the velocity immediately downstream of the shock waves

 

A supersonic air stream at 35 kPa is deflected by a wedgeshaped two-dimensional obstacle of total angle 20â—¦ mounted with its axis parallel to the oncoming flow. Shock waves are observed coming from the apex at 40â—¦ to the original flow direction. What is the initial Mach number and the pressure rise through the shocks? If the stagnation temperature is 30 â—¦C what is the velocity immediately downstream of the shock waves?

 

 

 
 

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Alpha Geek
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Status NEW Posted 23 May 2017 10:05 AM My Price 6.00

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file 1495534789-Answer.docx preview (122 words )
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