Designing and Simulating Compressible Flow in a Nozzle
V. Tapasvi1, M. Satyanarayana Gupta2, T. Kumaraswamy3
1V. Tapasvi, Department of Aeronautical, Jawaharlal Nehru Technological University, Hyderabad (Telangana), India.
2Dr. M. Satyanarayana Gupta, Department of Aeronautical, Jawaharlal Nehru Technological University, Hyderabad (Telangana), India.
3T. Kumaraswamy, Department of Aeronautical, Jawaharlal Nehru Technological University, Hyderabad (Telangana), India.
Manuscript received on 15 August 2015 | Revised Manuscript received on 25 August 2015 | Manuscript Published on 30 August 2015 | PP: 46-54 | Volume-4 Issue-6, August 2015 | Retrieval Number: F4162084615/15©BEIESP
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Abstract: Compressible flow is the branch of fluid mechanics that deals with flows having significant changes in fluid density. Gases, but not liquids, display such behavior. To distinguish between compressible and incompressible flow in gases, the Mach number must be greater than about 0.3 before significant compressibility occurs. A nozzle is a device designed to control the direction or characteristics of a fluid flow (especially to increase velocity) as it exits (or enters) an enclosed chamber or pipe. Now we are designing a nozzle by using a gambit design software and then converting that into a ansys software for analysis .In that analysis we are giving boundary conditions and inlet and outlet. This analysis totally on c-d nozzle. By using supersonic steam
Keywords: Fluid Mechanics, Density, Incompressible Flow, Mach Number, Compressibility, Fluid Flow
Scope of the Article: Solid Mechanics