Outputs for AEROSPACE ENGINEERING Department (Year 2016)
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Articles
- A hybrid optimal control approach to fuel-efficient aircraft conflict avoidance
- Analysis of the numerical diffusion in anisotropic mediums: benchmarks for magnetic field aligned meshes in space propulsion simulations
- Assessment of secondary bubble formation on a backward-facing step geometry
- Blob-enhanced reconstruction technique
- Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future
- Collocation methods to minimum-fuel trajectory problems with required time of arrival in ATM
- Determination of the force transmitted by an ion thruster plasma plume to an orbital object
- Effect of the plasma-induced magnetic field on a magnetic nozzle
- Ensemble 3D PTV for high resolution turbulent statistics
- Flow field features of fractal impinging jets at short nozzle to plate distances
- Fully magnetized plasma flow in a magnetic nozzle
- Heat transfer and thermal stresses in a circular tube with a non-uniform heat flux
- Influence of geometrical parameters on the linear stability of a Bénard-Marangoni problem
- Main results of the 4th International PIV Challenge
- Minimum induced drag theorems for joined wings, closed systems, and generic biwings: applications
- On the onset of horizontal convection
- Three-dimensional instabilities in the wake of a flapping wing at low Reynolds number
- Wake of tandem cylinders near a wall
Book Chapters
- Flow Field Topology of Impinging Jets with Fractal Inserts. In: Progress in Turbulence VI.
- Magnetic nozzles for space plasma thrusters. In: Encyclopedia of plasma technology
- Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings. In: Variational Analysis and Aerospace Engineering : Mathematical Challenges for the Aerospace of the Future
Conference Contributions
- A 3D Hybrid Code to Study Electric Thruster Plumes
- A numerical study of finite aspect ratio wings in flapping motion at low Reynolds
- ATM performance analysis in Madrid ACC sectors considering optimal aircraft trajectories
- Advanced Techniques for the Investigation of Flow Field and Heat Transfer in impinging Jets
- Analysis of Thermionic Bare Tether Operation Regimes in Passive Mode
- Analysis of the aerodynamic forces on heaving and pitching airfoils at low Reynolds number
- BETsMA: A Friendly Tool for Electrodynamic Tether Mission Design
- Collisionless electron cooling in unmagnetized plasma thruster plumes
- Comparison of technologies for de-orbiting spacecraft from Low-Earth-Orbit at end of mission
- DNS investigation of differential-diffusion effects on temporarily evolving turbulent diffusion flames
- Decomposing the aerodynamic forces of low-Reynolds flapping airfoils
- Deorbit with Bare Tether System from High Eccentricity Initial Orbit: Analyses and Numerical Simulations
- Development and Validation of a 2D Wave-Plasma Code for Helicon Plasma Thrusters
- Development of physical models of electron cooling in collisionless plasma thruster plumes
- Electron thermodynamics in the magnetized expansion of a rarefied plume
- Flow field characterization of round jets with fractal grid inserts
- Flow over flapping airfoils: qualitative and quantitative comparison between experiments and simulations
- Heuristic Method Based on Generalized Logarithmic Spirals for Low-Thrust Trajectory Design
- Horizonte ISDEFE: Espacio. Análisis del marco institucional y de las principales líneas de desarrollo e investigación actuales en el área Vigilancia y Seguimiento espaciales (SST)
- Hybrid Particle Codes for Electric Propulsion
- Hyperspectral tomography for aerospace plasma flow investigations
- Identifying Well-Behaved Turbulent Boundary Layers
- Identifying well-behaved turbulent boundary layers
- Ion Beam Shepherd Mission LEOSWEEP: mission design to ion beam thruster testing
- Kinetic modelling of collisionless electron cooling on magnetized plasma expansions
- Localization of Extreme Light: Relativistic Solitons, quasi-solitons and Breathers
- Low order modeling of forces and flow features in flapping wings
- Low order modeling of forces and flow features in flapping wings
- Maiden tests of the HPT05 helicon plasma thruster Prototype
- Modal decomposition of flow features in flapping wings and modes contribution to forces
- Modelling forces and flow features in flapping wings: a POD bases approach
- NOMADS: development of a versatile plasma discharge simulation plarform for electrinc propulsion
- Nonlinear structural modal model for aeroelastic applications
- On the canonical development of adverse-pressure-gradient turbulent boundary layers
- Patient-specific analysis of blood stasis in the left atrium
- Physics of magnetic nozzles for plasma thrusters
- Propellantless Technology for Deorbiting of Small Satellites Mega-Constellation at the End of Life
- Revisiting tripping effects in low-Reynolds number turbulent boundary layers
- Sequential Method to Compute Multiobjective Optimal Low-thrust Earth Orbit Transfer
- Simulación Numérica de Recolección de Corriente en una Sonda de Langmuir Cilíndrica
- Smart rotor: control of dynamic loads on a rotor blade
- Smart rotor: controlling dynamic stall by means of an actuated flap
- Studying the Plume Neutralization Process of the PEGASES thruster
- The flow around a flapping-wing micro air vehicle in free flight
- Thrust generation in heaving and flapping wings in forward flight
- Wind tunnel studies of history effects in turbulent boundary layers
- Wind-Based Robust Aircraft Route Optimization using Meteorological Ensemble Prediction Systems
- Wind-Based Robust Trajectory Optimization using Meteorological Ensemble Probabilistic Forecasts
Projects
- Aerial Refuelling Hose Guillotine Rig Test
- Aerodinámica del vuelo del avance de un micro-vehículo aéreo con dos pares de alas batientes: efectos tridimensionales, aeroelásticos y dinámica del vehículo
- Asesoramiento y seguimiento de tareas relacionadas con la obtención de datos ADSB, la decodificación de los mismos y métricas ATM
- CHEOPS: Consortium for Hall Effect Orbital Propulsion System
- Characterisation tests on Helicon Plasma Thruster
- Convenio específico entre Ingeniería de Sistemas para la Defensa de España y la Universidad Carlos III de Madrid para el desarrollo de actividades de prospectiva tecnológica en el ámbito aeroespacial, investigación y docencia de interés común - Trabajos de Prospectiva Tecnológica
- Development of an advanced axisymmetric model of the full plasma discharge in the Helicon Plasma Thruster
- E! - DEGASS - Desarrollo de sistemas embarcados de generación de gas inerte para aviones de tamaño medio y medio recorrido
- Model and experimental validation of spacecraft-thruster interactions (erosion) for electric propulsion thruster plumes
- PIV study of a flapping airfoil with an actuated Trailing Edge Flap
- Propulsores electromagnéticos para la exploración espacial
- Service Contract for supporting BR&TE in TAAM simulation and integration
- Servicios en el área de la gestión del tráfico aéreo para SENASA
- Simulación y ensayos en vuelo de cometas de tracción aplicadas a la generación de energía eólica
- TBO-MET: Meteorological Urcentainty Management for Trajectory Based Operations
- Transferencia de calor por convección y estructuras coherentes en capas límites turbulentas