Supersonic flow

Code verification/validation with respect to experimental data banks

Mechanical Engineering / Aerospace Engineering / Computational Complexity / Computational Fluid Dynamics / Mesh generation / Interaction / Boundary Layers / Flow Control / Comparative Study / Control Systems / Shock Waves / Turbulence modeling / Interactions / Quality Criteria / Hypersonic Flow / Unsteady flow / Three Dimensional / Supersonic flow / Boundary Layer / Shock Wave / Turbulence Model / Data Dissemination / Experimental Data / Compressible fluid / Interaction / Boundary Layers / Flow Control / Comparative Study / Control Systems / Shock Waves / Turbulence modeling / Interactions / Quality Criteria / Hypersonic Flow / Unsteady flow / Three Dimensional / Supersonic flow / Boundary Layer / Shock Wave / Turbulence Model / Data Dissemination / Experimental Data / Compressible fluid

Queima de Parafina em Matriz Celulósica com Óxido Nitroso em um Motor Híbrido de Injeção Vortical

Rocket Propulsion / Rocket/Missile Modeling and Flight Simulation / Hybrid Propulsion / Supersonic flow / Supersonic Aerodynamics / Numerical modeling of the processes within the combustion chamber of a solid propellant rocket engine during the stabilization of the design operation mode / Method of Characteristics / Thrust Vectoring / Numerical modeling of the processes within the combustion chamber of a solid propellant rocket engine during the stabilization of the design operation mode / Method of Characteristics / Thrust Vectoring
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