International Journal of Science and Research (IJSR)

International Journal of Science and Research (IJSR)
Open Access | Fully Refereed | Peer Reviewed

ISSN: 2319-7064




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Informative Article | Mechanical Engineering | India | Volume 10 Issue 9, September 2021


Testing of a Supersonic Nozzle with Supersonic Intake

G. Veeresh Kumar, M Naga Sailaja, Ravi Sandeep Kumar Kona


Abstract: In air breathing motors, ram jet motor takes the preeminent lead in working of the jets and rockets with supersonic velocities. Since these motors don't have moving parts, they can accomplish supersonic velocities with diminished loads. An endeavour is made to know the job of supersonic admission that add to the working of the ram jet. To know the impacts of the liquid stream in and encompassing the admission, a model of the admission is utilized as a test example in an open office to accomplish close to genuine flight conditions. The necessary channel stream speed of liquid is produced and forced on the model. The pressing factor impacts because of the shocks, mathematical requirements and its related execution qualities like the absolute pressing factor recuperation are noticed.


Keywords: Propulsion, TurboJet, Wind Tunnel, Pressure Difference, SuperSonic


Edition: Volume 10 Issue 9, September 2021,


Pages: 1522 - 1524


How to Cite this Article?

G. Veeresh Kumar, M Naga Sailaja, Ravi Sandeep Kumar Kona, "Testing of a Supersonic Nozzle with Supersonic Intake", International Journal of Science and Research (IJSR), https://www.ijsr.net/get_abstract.php?paper_id=SR21713140558, Volume 10 Issue 9, September 2021, 1522 - 1524

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