Essays about: "Compressible Flow"
Showing result 1 - 5 of 24 essays containing the words Compressible Flow.
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1. Thermal Analysis of Wave Energy Converter : Developing a Compact CHT Model for Operational Insights
University essay from Linköpings universitet/Mekanisk värmeteori och strömningsläraAbstract : Climate change is a critical global issue that continues to shape the way we understand and interact with the world around us. It is discussed more than ever before, especially in politics. READ MORE
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2. Rocket Jet Impinging on a Surface
University essay from KTH/Teknisk mekanikAbstract : With the continuous growth of the space industry and the introduction of reusable rockets, the number of rocket launches is expected to increase significantly in the following years. During rocket launching, the engine exhaust impinges on the launch structure producing a complex flow field. READ MORE
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3. Verification of the fluid dynamics modules of the multiphysics simulation framework MOOSE : A work to test a candidate software for molten salt reactor analysis
University essay from Uppsala universitet/Institutionen för fysik och astronomiAbstract : This is a report of a verification study of the multiphysics simulation framework MOOSE which was preformed at the company Seaborg Technologies. In the process of designing molten salt reactors there is a special need of making credible multiphysics simulations since the fuel is in motion. READ MORE
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4. Experimental pressure loss analysis in a mini tube for a fully developed turbulent airflow. : Mini channels of lengths 22.5 mm to 150 mm in length with a constant diameter of 1.5 mm
University essay from Linköpings universitet/Mekanisk värmeteori och strömningsläraAbstract : The cooling systems in a gas turbine are especially important as the turbine blades and vanes are exposed to extreme temperatures. The relatively cool air is extracted from the compressors and fed to the turbines to cool the turbine blades. READ MORE
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5. Development of a CFD Boundary Condition to Simulate a Perforated Surface
University essay from Umeå universitet/Institutionen för fysikAbstract : In aircraft with jet propulsion engine intakes at supersonic speed, strong pressure waves referred to as shockwaves occur, which may interact with any present boundary layers along the intake surface. The adverse pressure gradients associated with Shock Wave-Boundary Layer Interaction (SWBLI) may cause boundary layer flow separation, which can result in disturbances of the flow that can be harmful to the device or decrease engine performance. READ MORE