| Nome |
# |
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Numerical Simulation of Fluidic Thrust-Vectoring, file e384c42e-5378-d4b2-e053-9f05fe0a1d67
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1067
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Set of Boundary Conditions for Aerodynamic Design, file e384c42d-f364-d4b2-e053-9f05fe0a1d67
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808
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Studio e Controllo di Strutture Vorticose di Parete, file e384c42e-2215-d4b2-e053-9f05fe0a1d67
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635
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An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations, file e384c42d-e586-d4b2-e053-9f05fe0a1d67
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524
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A Pseudo-Compressibility Method for Solving Inverse Problems
based on the 3D Incompressible Euler Equations, file e384c42e-32e0-d4b2-e053-9f05fe0a1d67
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488
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INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION, file e384c42e-1cf1-d4b2-e053-9f05fe0a1d67
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433
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An Inverse Method of Designing the Cooling Passages of Turbine Blades Based on the Heat Adjoint Equation, file e384c42e-2cbe-d4b2-e053-9f05fe0a1d67
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267
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A viscous inverse method for aerodynamic design, file e384c42d-f2d8-d4b2-e053-9f05fe0a1d67
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248
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Point vortex model for asymmetric inviscid wakes past bluff bodies, file e384c42e-35c1-d4b2-e053-9f05fe0a1d67
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219
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Synthetic jet modeling for flow control applications, file e384c42d-feaa-d4b2-e053-9f05fe0a1d67
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195
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Nozzles and Intakes Interacting with the External Flow: Design and Analysis, file e384c42d-eed7-d4b2-e053-9f05fe0a1d67
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145
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Optimal Aerodynamic Design of Scramjet Facility Nozzles, file e384c430-3043-d4b2-e053-9f05fe0a1d67
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135
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Optimal Inverse Method for Turbomachinery Design, file e384c42d-f11f-d4b2-e053-9f05fe0a1d67
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123
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Active Flow Control in Supersonic Nozzles, file e384c430-38ba-d4b2-e053-9f05fe0a1d67
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123
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Integrated Design and Analysis of Intakes and Nozzles in Air-Breathing Engines, file e384c42d-e587-d4b2-e053-9f05fe0a1d67
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121
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A New Steklov-Poincaré Numerical Technique for Solving Prandtl-Batchelor Flows, file e384c430-303b-d4b2-e053-9f05fe0a1d67
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115
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Blade Camber Surface Optimization for Turbomachinery Design, file e384c42d-f122-d4b2-e053-9f05fe0a1d67
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79
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ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL, file e384c430-819d-d4b2-e053-9f05fe0a1d67
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64
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Numerical Investigation of the Dynamic Characteristics of a Dual-Throat-Nozzle for Fluidic Thrust-Vectoring, file e384c42f-4c3e-d4b2-e053-9f05fe0a1d67
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62
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A viscous inverse method for aerodynamic design, file e384c42d-f2d6-d4b2-e053-9f05fe0a1d67
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30
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An Aerodynamic Optimization Method based on the Inverse Problem Adjoint Equations, file e384c42d-e588-d4b2-e053-9f05fe0a1d67
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24
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Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike, file e384c433-52c4-d4b2-e053-9f05fe0a1d67
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21
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Numerical Simulation of a Vectored Axisymmetric Nozzle, file e384c432-c8a6-d4b2-e053-9f05fe0a1d67
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20
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Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method, file e384c434-27f3-d4b2-e053-9f05fe0a1d67
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18
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Multi-fidelity sparse polynomial chaos expansion based on Gaussian process regression and least angle regression, file e384c433-0ab4-d4b2-e053-9f05fe0a1d67
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13
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Characteristic-based formulation of boundary conditions for preconditioned or non-preconditioned flow equations, file e384c430-c7ef-d4b2-e053-9f05fe0a1d67
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12
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Parametric Generation and Computational Analysis of a REST Inlet, file e384c430-f5fa-d4b2-e053-9f05fe0a1d67
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12
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CFD-based Fluidic Thrust Vectoring model for fighter aircraft, file e384c430-f697-d4b2-e053-9f05fe0a1d67
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10
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A Comparison Of Different Technologies For Thrust Vectoring In A Linear Aerospike, file e384c433-db32-d4b2-e053-9f05fe0a1d67
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10
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AI Based Shock-Wave Detection by Using a Pressure Sensor Array, file e384c434-64f2-d4b2-e053-9f05fe0a1d67
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9
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Optimal aerodynamic design of hypersonic inlets by using streamline-tracing techniques, file e384c432-4138-d4b2-e053-9f05fe0a1d67
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8
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Reduced order modeling of thermal transients in high-performance engineering systems, file e384c430-c7f0-d4b2-e053-9f05fe0a1d67
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7
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A Numerical Method for the Study of Fluidic Thrust-Vectoring, file e384c42f-15f8-d4b2-e053-9f05fe0a1d67
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6
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Shock Vector Control Technique for Aerospike Nozzles, file e384c431-28e8-d4b2-e053-9f05fe0a1d67
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6
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Cold Gas Measurement System for Linear Aerospike Nozzles, file 65632998-4b9e-47bd-b128-b89749884867
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5
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Computational Investigation of Injection Effects on Shock Vector Control Performance, file e384c430-356e-d4b2-e053-9f05fe0a1d67
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5
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A fault/failure detection algorithm based on a grid of virtual sensors for engine health monitoring, file e384c431-085a-d4b2-e053-9f05fe0a1d67
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5
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A Pseudo-Compressibility Method for Solving Inverse Problems
based on the 3D Incompressible Euler Equations, file e384c42e-32e1-d4b2-e053-9f05fe0a1d67
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4
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A computational approach to the simulation of controlled flows by synthetic jets actuators, file e384c42e-34ff-d4b2-e053-9f05fe0a1d67
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4
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Design and Optimization of an Inward-Turning Inlet with Rectangular-To-Ellipse Shape Transition, file e384c431-09bd-d4b2-e053-9f05fe0a1d67
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4
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Fluidic Thrust Vectoring for Annular Aerospike Nozzle, file e384c432-6170-d4b2-e053-9f05fe0a1d67
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4
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Aerodynamic Design of Inward-Turning Inlets with Shape Transition, file e384c432-c8a7-d4b2-e053-9f05fe0a1d67
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4
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Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle, file e384c433-fd31-d4b2-e053-9f05fe0a1d67
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4
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Reduced order modelling of full-span rotating stall for the flow control simulation of axial compressors, file e384c42e-36f9-d4b2-e053-9f05fe0a1d67
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3
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The Clean Sky 2 MIDAS Project - an Innovative Modular, Digital and Integrated Air Data System for Fly-by-Wire Applications, file e384c430-e493-d4b2-e053-9f05fe0a1d67
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3
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Influence of the External Flow Conditions to the Jet-Vectoring Performances of a SVC Nozzle, file e384c431-01a3-d4b2-e053-9f05fe0a1d67
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3
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Sensitivity Analysis for Model with Dependent Inputs Using Sparse Polynomial Chaos Expansions, file e384c433-b7e8-d4b2-e053-9f05fe0a1d67
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3
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Stator re-stagger optimization in multistage axial compressor, file e384c433-c571-d4b2-e053-9f05fe0a1d67
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3
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A Vortex-In-Cell Method for the Simulation of Viscous Flows, file e384c42f-e501-d4b2-e053-9f05fe0a1d67
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2
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Numerical simulation of the unsteady flowfield in complete propulsion systems, file e384c430-2191-d4b2-e053-9f05fe0a1d67
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2
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Stator re-stagger optimization in multistage axial compressor, file e384c433-d110-d4b2-e053-9f05fe0a1d67
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2
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An improved stall prediction model for axial compressor stage based on diffuser analogy, file e384c434-d9d9-d4b2-e053-9f05fe0a1d67
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2
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Simulation of Jet Engine Transient by a CFD Method, file e384c42d-f396-d4b2-e053-9f05fe0a1d67
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1
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INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES BASED ON THE HEAT ADJOINT EQUATION, file e384c42e-1cf0-d4b2-e053-9f05fe0a1d67
|
1
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Point vortex model for asymmetric inviscid wakes past bluff bodies, file e384c42e-302c-d4b2-e053-9f05fe0a1d67
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1
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Open and Closed-Loop Responses of a Dual-Throat Nozzle during Fluidic Thrust Vectoring, file e384c42f-01f7-d4b2-e053-9f05fe0a1d67
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1
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Numerical Simulation of Fluidic Thrust-Vectoring, file e384c42f-45c8-d4b2-e053-9f05fe0a1d67
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1
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Design and Testing of a Low-Cost Extended-Range Pressure Measurement System for Aerospace Applications, file e384c42f-8b60-d4b2-e053-9f05fe0a1d67
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1
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On the Use of Synthetic Jet Actuators to Induce Jet-Vectoring in Nozzles, file e384c42f-e182-d4b2-e053-9f05fe0a1d67
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1
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Influence of the Facility Nozzle Design in the Unsteady Response of Direct-Connect Scramjet Combustors, file e384c42f-e335-d4b2-e053-9f05fe0a1d67
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1
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Inverse Problems for Advanced Nozzle Design., file e384c431-165a-d4b2-e053-9f05fe0a1d67
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1
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Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle, file e384c433-fd30-d4b2-e053-9f05fe0a1d67
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1
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Numerical Investigation of the Burner-Nozzle Interaction on Fluidic Thrust Vectoring, file e384c434-cead-d4b2-e053-9f05fe0a1d67
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1
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| Totale |
6130 |
Archivio Istituzionale della Ricerca