Design the 2D steady MOC contour for a super sonic nozzle assuming that the expansion section is a simple corner of some fixed angle, with the straightening section being designed to produce uniform outflow. The inflow for your nozzle is to be M = 1, gamma = 1.4, P = 101325, T = 300K, incoming flow area of 1m, with 1m depth into the page. The exit Mach number of your design is to be M = 3. Note to execute this properly you will need to compute v (nu) as a function of M, and viceversa. Please use Matlab for results.

Design the 2D steady MOC contour for a super sonic nozzle assuming that the expansion section is a simple corner of some fixed angle, with the straightening section being designed to produce uniform outflow. The inflow for your nozzle is to be M = 1, gamma = 1.4, P = 101325, T = 300K, incoming flow area of 1m, with 1m depth into the page. The exit Mach number of your design is to be M = 3. Note to execute this properly you will need to compute v (nu) as a function of M, and viceversa. Please use Matlab for results.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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