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By using the method of characteristics write a matlab code to design a minimum length rocket nozzle with the following input parameters: Total temperature in
By using the method of characteristics write a matlab code to design a minimum length rocket nozzle with the following input parameters:
Total temperature in combustion chamber Tt=3000 [K] Total pressure in combustion chamber pt=1500 [kPa]
Mass flow rate through the nozzle m = 10kg / s Contour plot your solution ( Mach, pressure,
temperature, density, velocity magnitude)
using matlab.
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Lncs 8999 Databases In Networked Information Systems 10th International Workshop Dnis 2015 Aizu Wakamatsu Japan March 23 25 2015 Proceedings
Authors: Wanming Chu ,Shinji Kikuchi ,Subhash Bhalla
2015th Edition
3319163124, 978-3319163123
