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20092022
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Research Output 2009 2018

2018

Ice accretion effects on helicopter rotor performance, via multibody and CFD approaches

Kelly, D., Habashi, W. G., Quaranta, G., Masarati, P. & Fossati, M., 31 May 2018, In : Journal of Aircraft. 55, 3, p. 1165-1176 12 p.

Research output: Contribution to journalArticle

Open Access
File
Helicopter rotors
Flight dynamics
Ice
Aerodynamics
Computational fluid dynamics

Preface to the special issue on: "29th international conference on parallel computational fluid dynamics"

Drikakis, D., Fossati, M., Kazakidi, A. & Emerson, D. R., 15 Oct 2018, In : Computers and Fluids. 175, p. 1 1 p.

Research output: Contribution to journalEditorial

Open Access
File
2017

Finite element modeling of nonequilibrium fluid-wall interaction at high-Mach regime

Dumas, M-E., Habashi, W. G., Baruzzi, G. S., Isola, D. & Fossati, M., 30 Nov 2017, In : Journal of Aircraft. 54, 6, p. 2330-2339 10 p.

Research output: Contribution to journalArticle

Open Access
File
Mach number
Fluids
Navier Stokes equations
Aerodynamics
Temperature

Finite element modeling of non-equilibrium fluid-wall interaction beyond the continuum regime

Dumas, M-E., Habashi, W., Isola, D., Baruzzi, G. & Fossati, M., 24 Mar 2017, (Accepted/In press) In : Journal of Aircraft.

Research output: Contribution to journalArticle

Open Access
File
Fluids
Navier Stokes equations
Mach number
Aerodynamics
Temperature

Ice accretion effects in helicopter rotor performance via multi-body and CFD approaches

Kelly, D., Habashi, W. G., Quaranta, G., Masarati, P. & Fossati, M., 24 Sep 2017, (Accepted/In press) In : Journal of Aircraft.

Research output: Contribution to journalArticle

Open Access
File
Helicopter rotors
Flight dynamics
Ice
Aerodynamics
Computational fluid dynamics

Modeling scramjet supersonic combustion via Eddy Dissipation Model

Hoste, J-J. O. E., Fossati, M., Taylor, I. J. & Gollan, R. J., 25 Sep 2017. 13 p.

Research output: Contribution to conferencePaper

Open Access
File
Reusability
Mach number
Computational fluid dynamics
Orbits
Turbulence

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 proceedingConference contribution

Open Access
File
supersonic combustion ramjet engines
supersonic flow
Supersonic flow
propulsion
Propulsion

Shock-conforming mesh generation for aerodynamic analyses at supersonic regimes

Herrera Montojo, J., Fossati, M. & Minisci, E., 3 Nov 2017, In : Computers and Fluids. 157, p. 276-293 18 p.

Research output: Contribution to journalArticle

Open Access
File
Mesh generation
Supersonic flow
Shock waves
Aerodynamics
Hypersonic vehicles
2016
2 Citations

A Jacobian-free edged-based Galerkin formulation for compressible flows

Gao, S., Habashi, W. G., Isola, D., Baruzzi, G. S. & Fossati, M., 26 Oct 2016, In : Computers and Fluids.

Research output: Contribution to journalArticle

Open Access
File
Supersonic flow
Compressible flow
Mach number
Subsonic flow
Hypersonic flow

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 proceedingConference contribution

Atmospheric density
Civil aviation
Fluids
Flow velocity
Navier Stokes equations
1 Citations

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 proceedingConference contribution

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 proceedingConference contribution

Fuel sloshing
Navier Stokes equations
Ice
Stabilization
Water

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 proceedingConference contribution

detachment
droplet
splashing
geometry
ice formation
computational fluid dynamics
Computational fluid dynamics
Physics
Biomedical engineering
Mechanical engineering

Quasi-molecular modeling of single supercooled large droplet impact

Abdollahi, V., Habashi, W. G., Baruzzi, G. S. & Fossati, M., 30 Apr 2016, In : Applied Mathematical Modelling. 40, 7-8, p. 4560 - 4571 12 p.

Research output: Contribution to journalArticle

Molecular Modeling
Molecular modeling
Droplet
Molecules
Water
4 Citations

Real-time regional jet comprehensive aeroicing analysis via reduced order modeling

Zhan, Z., Habashi, W. G. & Fossati, M., 20 Jul 2016, In : AIAA Journal. 54, 12, p. 3787-3802 16 p.

Research output: Contribution to journalArticle

Open Access
File
Learning algorithms
Aviation
Ice
Drag
Learning systems
2015
3 Citations

A 3D mesh deformation technique for irregular in-flight ice accretion

Pendenza, A., Habashi, W. G. & Fossati, M., 20 Oct 2015, In : International Journal of Numerical Methods in Fluids. 79, 5, p. 215-242 28 p.

Research output: Contribution to journalArticle

Mesh Deformation
Accretion
Airports
Ice
Irregular
1 Citations

A hybrid Taylor-Galerkin variational multi- scale stabilization method for the level set equation

Bakkar, A., Habashi, W. G., Fossati, M. & Baruzzi, G. S., 22 Oct 2015, In : Computers and Fluids. 121, p. 192-205 14 p.

Research output: Contribution to journalArticle

Stabilization
Taylor series
Ice problems
Advection
Stretching

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 proceedingConference contribution

Hypersonic aerodynamics
Conservation
Thermodynamics
8 Citations

Eulerian modeling of supercooled large droplet splashing and bouncing

Bilodeau, D., Habashi, W., Baruzzi, G. & Fossati, M., 30 Sep 2015, In : Journal of Aircraft. 52, 5, p. 1611 - 1624 14 p.

Research output: Contribution to journalArticle

Airfoils
Conservation
Aerodynamics
Aircraft
Geometry
11 Citations

Evaluation of aerodynamic loads via reduced order methodology

Fossati, M., 31 Aug 2015, In : AIAA Journal. 53, 8, p. 2389-2405 17 p.

Research output: Contribution to journalArticle

Aerodynamic loads
Decomposition
Subsonic flow
Fixed wings
Transonic flow
8 Citations

Local reduced order modeling and iterative sampling for parametric analyses of aero-icing problems

Zhan, Z., Habashi, W. G. & Fossati, M., 31 Aug 2015, In : AIAA Journal. 53, 8, p. 2174 - 2185 10 p.

Research output: Contribution to journalArticle

Learning algorithms
Sampling
Unsupervised learning
Supervised learning
Learning systems

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 proceedingConference contribution

Ice
Swept wings
Airfoils
Numerical methods
Topology
2014
2 Citations

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 proceedingConference contribution

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 proceedingConference contribution

Ice
Helicopter rotors
Computational fluid dynamics
Rotors
Flight dynamics

The Riemann problem for hyperbolic equations under a nonconvex flux with two inflection points

Fossati, M. & Quartapelle, L., 24 Feb 2014, [Ithaca, NY], 104 p.

Research output: Working paper

Fluxes
Gases
Euler equations
Nonlinear equations
Specific heat
2013
4 Citations

A kinetic node-pair formulation for two-dimensional flows from continuum to transitional regime

Fossati, M., Guardone, A., Vigevano, L. & Xu, K., 2013, In : AIAA Journal. 51, 4, p. 784-796 13 p.

Research output: Contribution to journalArticle

Kinetic theory of gases
Kinetics
Distribution functions
Conservation
Boundary conditions
3 Citations

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 proceedingConference contribution

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 proceedingConference contribution

Aerodynamics
Computational fluid dynamics
Rotors
Decomposition
Interpolation
15 Citations

Multi-parameter analysis of aero-icing problems via proper orthogonal decomposition and multidimensional interpolation

Fossati, M. & Habashi, W. G., 2013, In : AIAA Journal. 51, 4, p. 946-960 15 p.

Research output: Contribution to journalArticle

Interpolation
Decomposition
Eigenvalues and eigenfunctions
Computer simulation
4 Citations

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 proceedingConference contribution

ice formation
droplet
flight
splashing
flight conditions
2012
17 Citations

An ALE mesh movement scheme for long-term in-flight ice accretion

Fossati, M., Khurram, R. A. & Habashi, W. G., 20 Mar 2012, In : International Journal of Numerical Methods in Fluids. 68, 8, p. 958 - 976 19 p.

Research output: Contribution to journalArticle

Accretion
Mesh Deformation
Ice
Glazes
Mesh
2 Citations

A node-pair finite element/volume mesh adaptation technique for compressible flows based on a hierarchical approach

Fossati, M., Guardone, A. & Vigevano, L., 20 Nov 2012, In : International Journal of Numerical Methods in Fluids. 70, 8, p. 1004-1026 23 p.

Research output: Contribution to journalArticle

Finite Volume Element
Mesh Adaptation
Compressible flow
Coarsening
Compressible Flow
8 Citations

Simulation of supercooled large droplet impingement via reduced order technology

Fossati, M., Habashi, W. G. & Baruzzi, G. S., 31 Mar 2012, In : Journal of Aircraft. 49, 2, p. 600 - 610 11 p.

Research output: Contribution to journalArticle

2011
3 Citations

FENSAP-ICE: numerical prediction of ice roughness evolution, and its effects on ice shapes

Ozcer, I. A., Baruzzi, G. S., Reid, T., Habashi, W. G., Fossati, M. & Croce, G., 1 Dec 2011.

Research output: Contribution to conferencePaper

Ice
Surface roughness
Steady flow
Airfoils
Water content
1 Citations

Impingement of supercooled large droplets via reduced order models

Fossati, M., Habashi, W. G. & Baruzzi, G., 1 Dec 2011.

Research output: Contribution to conferencePaper

Computational fluid dynamics
Aircraft
Interpolation
Decomposition
Costs
4 Citations

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 proceedingConference contribution

Viscous flow
Airfoils
Mach number
Wind tunnels
Tensors
2 Citations

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 proceedingConference contribution

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 proceedingConference contribution

Kinetic theory of gases
hypersonic flow
Hypersonic aerodynamics
Conservation
Fluxes
1 Citations

Robust moving meshes for the prediction of aerodynamic degradation during in-flight icing

Fossati, M., Khurram, R. U. A. & Habashi, W. G., 13 Jun 2011.

Research output: Contribution to conferencePaper

Ice
Aerodynamics
Degradation
Glazes
Heat flux
2010
4 Citations

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 proceedingConference contribution

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 proceedingConference contribution

Knudsen flow
BGK model
compressible flow
formulations
kinetics
19 Citations

Hybrid grid generation for two-dimensional high-Reynolds flows

Dussin, D., Fossati, M., Guardone, A. & Vigevano, L., 2009, In : Computers and Fluids. 38, 10, p. 1863-1875 13 p.

Research output: Contribution to journalArticle

Mesh generation
Compressible flow
Viscous flow
Airfoils
Boundary layers