Research Output per year
Research Output 2009 2019
2017
Finite-element formulation of a Jacobian-free solver for supersonic viscous flows on hybrid grids
Gao, S., Habashi, W. G., Fossati, M., Isola, D. & Baruzzi, G. S., 5 Jan 2017, 55th AIAA Aerospace Sciences Meeting. Grapevine, Texas, p. 1-28 28 p. (AIAA SciTech Forum).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Open Access
File
Viscous flow
Mach number
Supersonic flow
Newton-Raphson method
Linear systems
Numerical modeling and simulation of supersonic flows in propulsion systems by open-source solvers
Hoste, J. J. O. E., Casseau, V., Fossati, M., Taylor, I. J. & Gollan, R. J., 3 Apr 2017, 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017. 17 p. 2411Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Open Access
File
supersonic combustion ramjet engines
supersonic flow
Supersonic flow
propulsion
Propulsion
2016
Finite element modeling of non-equilibrium fluid-wall interaction beyond the continuum regime
Dumas, M. E., Habashi, W. G., Fossati, M., Baruzzi, G. S. & Isola, D., 8 Jan 2016, 54th AIAA Aerospace Sciences Meeting.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Atmospheric density
Civil aviation
Fluids
Flow velocity
Navier Stokes equations
1
Citation
(Scopus)
Hybrid quasi molecular-continuum modeling of supercooled large droplet dynamics for in-flight icing conditions
Abdollahi, V., Habashi, W. G. & Fossati, M., 8 Jan 2016, 54th AIAA Aerospace Sciences Meeting.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Molecules
Water
Agglomeration
Liquids
Temperature
Modeling of large droplets impingement using a hybrid Taylor-Galerkin Variational Multi-Scale stabilized level set method
Bakkar, A., Habashi, W. G. & Fossati, M., 8 Jan 2016, 54th AIAA Aerospace Sciences Meeting.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Fuel sloshing
Navier Stokes equations
Ice
Stabilization
Water
2
Citations
(Scopus)
Numerical modeling of first and second order SLD effects on 3D geometries
Bilodeau, D. R., Habashi, W., Fossati, M. & Baruzzi, G., 17 Jun 2016, 8th AIAA Atmospheric and Space Environments Conference. WashingtonResearch output: Chapter in Book/Report/Conference proceeding › Conference contribution book
detachment
droplet
splashing
geometry
ice formation
2015
Development of a Jacobian-free finite element solver for aerothermodynamic design
Gao, S., Habashi, W. G., Fossati, M., Isola, D., Baruzzi, G. S. & Ozcer, I. A., 2015, 53rd AIAA Aerospace Sciences Meeting. 14 p.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Hypersonic aerodynamics
Conservation
Thermodynamics
Optimization of the Morphogenetic approach for in-flight icing
Butnarasu, M. C., Habashi, W. G. & Fossati, M., 2015, 53rd AIAA Aerospace Sciences Meeting. 10 p.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Ice
Swept wings
Airfoils
Numerical methods
Topology
2014
A 3D mesh deformation technique for irregular in-flight ice accretion shapes
Pendenza, A., Habashi, W. G. & Fossati, M., 2014, 44th AIAA Fluid Dynamics Conference.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Ice
Fluid structure interaction
Fluids
Assessment of ice accretion effects on rotor dynamics via multi-body and CFD approaches
Kelly, D., Fouladi, H., Fossati, M., Habashi, W. G., Alicino, R., Quaranta, G. & Masarati, P., 2014, Annual Forum Proceedings - AHS International. Vol. 3. p. 1840-1851 12 p.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Ice
Helicopter rotors
Computational fluid dynamics
Rotors
Flight dynamics
2013
An Eulerian re-impingement model of splashing and bouncing supercooled large droplets
Bilodeau, D. R., Habashi, W. G., Fossati, M. & Baruzzi, G. S., 2013, 5th AIAA Atmospheric and Space Environments Conference, Fluid Dynamics and Co-located Conferences.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
splashing
impingement
numerical method
droplet
geometry
A reduced order methodology for the parametric analysis of rotor aerodynamics
Fossati, M., Habashi, W. G., Biava, M. & Vigevano, L., 31 Jul 2013, 38th European Rotorcraft Forum 2012, ERF 2012. Amsterdam, Vol. 2. p. 1042-1055 14 p.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Aerodynamics
Computational fluid dynamics
Rotors
Decomposition
Interpolation
Quasi-molecular modeling of supercooled large droplets dynamics for in-flight icing simulations
Abdollahi, V., Habashi, W. G., Fossati, M. & Baruzzi, G. S., 2013, 5th AIAA Atmospheric and Space Environments Conference.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
ice formation
droplet
flight
splashing
flight conditions
2011
4
Citations
(Scopus)
Improved transient-fixed-point mesh adaptation using orthogonality-preserving metric intersection
Najafiyazdi, M., Habashi, W. G. & Fossati, M., 1 Dec 2011, 20th AIAA Computational Fluid Dynamics Conference 2011. Red Hook, NYResearch output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Viscous flow
Airfoils
Mach number
Wind tunnels
Tensors
Mesh adaptation for unsteady problems via reduced order modeling
Fossati, M., Najafiyazdi, M. & Habashi, W. G., 1 Dec 2011, 20th AIAA Computational Fluid Dynamics Conference 2011. 19 p.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Costs
Computational fluid dynamics
Numerical simulation of hypersonic transitional flows by means of a kinetic node-pair approach
Fossati, M., Vigevano, L. & Xu, K., 1 Dec 2011, 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Kinetic theory of gases
hypersonic flow
Hypersonic aerodynamics
Conservation
Fluxes
2010
A node-pair finite element / finite volume mesh adaptation technique for compressible flows
Fossati, M., Guardone, A. & Vigevano, L., 2 Dec 2010, 40th AIAA Fluid Dynamics Conference. 18 p. 2010-4438Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Compressible flow
Coarsening
Error analysis
Data structures
Experiments
2009
A node-pair bgk kinetic scheme for flows at moderate knudsen numbers
Fossati, M. & Vigevano, L., 17 Jun 2009, Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles. Vol. 659 SP.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book
Knudsen flow
BGK model
compressible flow
formulations
kinetics