Search for dissertations about: "Shock Boundary Layer Interaction"
Showing result 1 - 5 of 15 swedish dissertations containing the words Shock Boundary Layer Interaction.
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1. Numerical and Experimental study of shock boundary layer interaction in unsteady transonic flow
Abstract : A prerequisite for aeroelastic stability prediction inturbomachines is the understanding of the fluctuatingaerodynamic forces acting on the blades. Unsteady transonicflows are complex because of mutual interactions betweentravelling pressure waves, outlet disturbances, shock motion,and fluctuating turbulent boundary layers. READ MORE
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2. Large eddy simulation of transonic flow with shock wave/turbulent boundary layer interaction
Abstract : Large eddy simulations (LES) of shock wave/turbulent boundary layer interaction (SWTBLI) have been carried out. The flow configuration was that of transonic flow over a bump with inlet Mach number 0.75 and maximum Mach number 1.27. READ MORE
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3. Supersonic flow separation with application to rocket engine nozzles
Abstract : The increasing demand for higher performance in rocketlaunchers promotes the development of nozzles with higherperformance, which basically is achieved by increasing theexpansion ratio. However, this may lead to flow separation andensuing instationary, asymmetric forces, so-called side-loads,which may present life-limiting constraints on both the nozzleitself and other engine components. READ MORE
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4. Flow Processes in Rocket Engine Nozzles with Focus on Flow Separation and Side-Loads
Abstract : .... READ MORE
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5. Hot wire and PIV studies of transonic turbulent wall-bounded flows
Abstract : The compressible turbulent boundary layer developing over atwo-dimensional bump which leads to a supersonic pocket with aterminating shock wave has been studied. The measurements havebeen made with hot-wire anemometry and Particle ImageVelocimetry (PIV). READ MORE