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Marco Fossati

Dr

 https://orcid.org/0000-0002-1165-5825

  • United Kingdom

Accepting PhD Students

PhD projects

Reduced Basis Modeling for transonic aerodynamics High-Mach flows and nonequilibrium aerodynamics PH mesh adaptivity and (re)generation

20092022
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Research Output 2009 2019

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Conference contribution book
2017
1 Citation (Scopus)
1 Downloads (Pure)

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
175 Downloads (Pure)

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. 2411

Research 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
1 Citation (Scopus)

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. Washington

Research 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
3 Citations (Scopus)

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
4 Citations (Scopus)

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
4 Citations (Scopus)

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, NY

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book

Viscous flow
Airfoils
Mach number
Wind tunnels
Tensors
2 Citations (Scopus)

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
4 Citations (Scopus)

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. 2010-4438

Research 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