Current Organizations / Institutes

The organizations/institutes from the scholar's latest article

Previous Organizations / Institutes

The organizations / institutes from the scholar's other articles in the past ten years


Andrea Ferrero has a total of 93 co-authors. Here are the top co-authors by number of shared publications:


Latest Publications

  • Open Access

    Characterizing cryogenic chilldown and boil-off: A liquid nitrogen experimental study

    by Alessandra Zumbo, Andrea Ferrero, Filippo Masseni, Dario Pastrone

  • Open Access

    Euler-Lagrange modeling of circular discrete orifices gas-liquid pintle injectors using blob injection

    by Leonardo Stumpo, Andrea Ferrero, Filippo Masseni, Dario Pastrone

  • Open Access

    Characterizing Cryogenic Chilldown and Boil-Off: A Liquid Nitrogen Experimental Study

    by Alessandra Zumbo, Andrea Ferrero, Filippo Masseni, Dario Pastrone

    Cryogenic chilldown and boil-off directly impact the efficiency, safety and operational margins of any system that handles cryogenic fluids, including propulsion, storage and transfer applications. These processes arise from the interaction between wall heat transfer, boiling regimes, and vapor-space dynamics, and are strongly influenced by geometry, initial thermal conditions, and operating procedures. As a result, well-resolved experimental data remain essential for the development and validation of transient two-phase models. This work presents an experimental investigation of liquid nitrogen chilldown and boil-off in a small-scale test facility composed of two cryogenic vessels, a feed tank and a return tank, connected by a horizontal transfer line. The setup is instrumented to measure temperature evolution, pressure and liquid levels, under controlled valve operations. Wall heat fluxes and mass flow rates are derived from these measurements through energy and mass balances. The influence of initial thermal conditions is examined by comparing chilldown into a pre-cooled transfer line with that of an ambient-temperature configuration under unpressurised flow. To assess the role of the driving mechanism, both unpressurised and pressurised flow transfer conditions are then considered for an ambient temperature transfer line and return tank. Boil-off behaviour in the feed tank is characterized at different liquid fill levels and further investigated through controlled heating using an immersed electrical heater. The resulting dataset offers experimental observations useful for studying chilldown transients, two-phase flow, and tank boil-off.

  • Open Access

    Experimental and numerical validation of a multi-fidelity model for TPMS lattice heat exchangers based on porous media approximation

    by Alessandro Chiodi, Alessandro Alaia, Andrea Ferrero, Shahrokh Shahpar

    This work describes the experimental and numerical validation of a Multi-Fidelity (MF) model for the efficient simulation of Heat Exchangers (HX) based on Triply Periodic Minimal Surface (TPMS) lattices. The MF model is based on the porous media approximation developed in our previous work, where the porous lattice is modelled as a homogeneous medium characterised by variable permeability, Forchheimer, and heat transfer coefficients. Lattice coefficients are assumed to be dependent on the local lattice geometry and flow conditions, and are computed by a Machine Learning (ML) model. The ML model is trained on a database of LF simulations performed on individual lattice cells and a handful of High-Fidelity (HF) runs data. The resulting framework allows to run simulations at a fraction of the computational cost of a full-resolution CFD simulation. The validation of the proposed model is performed against both HF Conjugate Heat Transfer (CHT) simulations and experimental data. Experiments are performed on a series of Additively Manufactured (AM) HXs, tested under controlled thermal Boundary Conditions (BCs), at different inlet mass flow rates. Comparison with experimental data shows an excellent agreement for temperature distribution. A qualitative comparison with experimental measurements indicates that also the pressure drop is predicted correctly by the MF model. In particular, the MF model is able to capture the order of magnitude of the pressure drop and the overall trend with respect to the inlet mass flow rate. These results confirm the accuracy of the MF surrogate model and demonstrate that the proposed approach provides a reliable and computationally efficient tool for the simulation and optimisation of TPMS-based lattice HXs.

  • Open Access

    Reduced-Order Modeling and Active Subspace to Support Shape Optimization of Centrifugal Pumps

    by Giacomo Gedda, Andrea Ferrero, Filippo Masseni, Massimo Mariani, Dario Pastrone

    This study presents a reduced-order modeling framework for the shape optimization of a centrifugal pump. A database of CFD solutions is generated using Latin Hypercube Sampling over five design parameters to construct a reduced-order model based on proper orthogonal decomposition with radial basis function interpolation. The model predicts the flow field at the impeller–diffuser interface and pump outlet, enabling the estimation of impeller torque and total pressure rise. The active subspaces method is applied to reduce the dimensionality of the input space from five to four modified parameters. The sensitivity of the ROM is assessed with respect to further dimensionality reductions in the parameter space, POD mode truncation, and adaptive sampling. The model is then used to perform pump shape optimization via a quasi-Newton method, identifying the combination of the parameters that minimizes the impeller torque while satisfying a constraint on the head. The optimal result is validated through CFD analysis and compared against the Pareto front generated by a genetic algorithm. The work highlights the potential of model-order reduction techniques in centrifugal pump optimization.


  • Open Access

    Inverse Design of Additive Manufactured Rocket Propellant Grains with Non-Uniform Properties

    by Giovanni Polizzi, Andrea Ferrero, Filippo Masseni, Dario Pastrone

    This work explores solid rocket motor grain design, leveraging additive manufacturing techniques based on slurry deposition and UV-curing. The objective is to develop an automated design procedure to identify optimal solutions that meet mission requirements, exploiting new geometries and ballistic configurations previously unattainable with the classical mix–cast–cure manufacturing process. The design procedure is based on a stochastic optimization approach coupled with surrogate modeling of the pressure–time response, considering variable geometrical and ballistic parameters. Several surrogate models were tested after the creation of suitable databases through the computation of pressure evolution for different configurations. The most appropriate surrogate model was selected and applied within optimization routines to evaluate individual designs. The optimizer identifies the most suitable configuration to obtain the desired pressure–time response and to meet motor requirements. Different design approaches have been tested to evaluate the ballistic distribution’s influence on performance and how it can be leveraged to meet requirements, even with significant modifications in grain geometry. The results show that the proposed procedure is able to effectively achieve the expressed requirements, successfully handling the novel design environment. Furthermore, they highlight the strong influence of the ballistic distribution on performance and show how it can be successfully exploited to guide grain design.


  • Open Access

    A Chemical Reactor Network methodology for estimating NO x emissions under non-premixed lean hydrogen combustion with water injection

    by Lorenzo Folcarelli, Riccardo Concetti, Fabio Cozzi, Andrea Ferrero, Filippo Masseni, Dario Pastrone, Josef Hasslberger, Markus Klein


  • Open Access

    Evaluation of UV-Curable Solid Rocket Propellants’ Properties for Advanced 3D Printing Technologies

    by Filippo Masseni, Giacomo Tetti, Alessandra Zumbo, Camilla Noé, Giovanni Polizzi, Leonardo Stumpo, Andrea Ferrero, Dario Pastrone

    Challenges in the traditional cast-and-cure manufacturing of composite solid propellants, such as the use of mandrels and the toxicity of curing agents, are being addressed through new propellant formulations and additive manufacturing techniques. Within this framework, this study aimed to investigate the properties of UV-curable composite solid rocket propellants, focusing on their compatibility with advanced 3D printing technologies. Polybutadiene-based propellants incorporating a specific photoinitiator were examined. Key rheological properties, including the pseudoplasticity and pot-life, were assessed to evaluate the material’s behavior during the printing process. Furthermore, photopolymerization tests were performed using a customized delta illuminator to evaluate the conversion efficiency under UVA and UVC light sources. Concurrently, a modular Cartesian 3D printer was developed and preliminary tests were performed. Rheological tests also revealed a flow index n of 0.32 at 60 °C and 0.46 at 80 °C, indicating significant pseudoplastic behavior. The pot-life tests showed that the viscosity of the propellant reached the upper limit of 106 cP more quickly at higher temperatures, indicating a shorter time range of printability. UVA irradiation resulted in a polymerization conversion rate of about 90%, while UVC exposure did not significantly enhance the conversion rate beyond this value. Finally, the 3D printing tests confirmed the feasibility of producing solid propellant, though challenges related to material segregation and the extrusion consistency were observed. Material separation resulted in a significant impact on the printability, causing underextrusion and nozzle clogging, particularly with smaller nozzle diameters and higher extrusion pressures. Overall, this research represents a significant step forward in the development of UV-curable propellants for additive manufacturing, building on previous advancements by the research group. It demonstrates tangible progress in addressing key challenges such as the printability, material performance, and curing efficiency, while also highlighting areas requiring further refinement. These findings underscore the continuous evolution of this technology toward higher readiness levels, paving the way for its broader application in composite solid propellant manufacturing.