Categoria: NICFD

  • AeroPhD Seminars

    AeroPhD Seminars

    Prof. Iaccarino (Stanford University), Prof. Luchini (Università di Salerno) and Prof. Pirozzoli (Sapienza Università di Roma) will present the latest findings in fluid mechanics, discussing on ensemble computing, universality law for turbulent flows and turbulent channel flows in complex geometries in seminars that will be held on Monday January 21st at Aerospace Department of Politecnico di Milano.

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  • PhD defence

    On Monday January 28th at 9.00 am in Sala Consiglio of DAER, Giulio Gori and Davide Vimercati will defend their PhD thesis. The committe is composed by Franco Auteri, Gianluca Iaccarino, Sergio Pirozzoli, Paolo Luchini and Edward Cox.

     

    NON-IDEAL STEADY SUPERSONIC FLOWS

    Davide Vimercati

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    NON-IDEAL COMPRESSIBLE-FLUID DYNAMICS: DEVELOPING A COMBINED PERSPECTIVE ON MODELING, NUMERICS AND EXPERIMENTS

    Giulio Gori

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  • NICFD 2018 schedule

    NICFD 2018 schedule

    It is now available the full schedule of the NICFD conference.

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  • JOIN US AT NICFD 2018

    JOIN US AT NICFD 2018

    It is our great pleasure to welcome you to the 2nd International Seminar on Non-Ideal Compressible-Fluid Dynamics for Propulsion & Power, which will be held on the 4th and 5th of October 2018 in Bochum, Germany.

    NICFD 2018 is intended to promote the exchange of scientific information, to encourage and consolidate the interaction between researchers and professionals, with a special emphasis on the progress in research, development, and applications of the topics related to the field of propulsion and power.

    The themes range from the theoretical foundations to advanced numerical and experimental practices and applied technologies. The conference provides an exciting opportunity to share, learn and discuss the latest insights.

    The conference is organised by Prof. Francesca di Mare (Thermal Turbomachines and Aeroengines, Ruhr-Universität Bochum), Prof. Andrea Spinelli (CREALab, Politecnico di Milano) and Prof. Matteo Pini (Propulsion & Power, TUDelft).

    Further infomation can be found on the flyer and on the website.

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  • Presentation of experimental results from TROVA at ORC 2017

    Presentation of experimental results from TROVA at ORC 2017

    221 – Experimental observation of non-ideal expanding flows of Siloxane MDM vapor for ORC applications 
    by Andrea Spinelli, Giorgia Cammi, Marta Zocca, Simone Gallarini, Fabio Cozzi, Paolo Gaetani, Vincenzo Dossena, Alberto Guardone
    Session 4C, Thursday at 14.20

     

    Abstract: Extensive experimental results characterizing the supersonic expansion of an organic vapor in non-ideal conditions are reported in this paper for the first time. The collected data also allowed the assessment of the accuracy of Computational Fluid Dynamic (CFD) tools employed to predict the non-ideal behavior of such flows, including the consistency of thermodynamic models adopted. The investigation has been carried out on the converging-diverging nozzle test section of the Test Rig for Organic VApors (TROVA), at the Laboratory of Compressible fluid-dynamics for Renewable Energy Application (CREA) of Politecnico di Milano. Supersonic nozzle flow has been chosen as the simplest one of significance for organic Rankine cycle (ORC) turbine channels. The working fluid under scrutiny is Siloxane MDM, a widely employed compound for high temperature ORCs. MDM vapor expands through the TROVA nozzle at moderate non-ideal conditions in the close proximity of the vapor saturation curve. This is the region where ORC expanders typically operate, thus proving the relevance of the investigation for the ORC community. Indeed, detailed experimental data representative of typical ORC expansions were lacking in the open literature up to date. Two different nozzle geometries, featuring exit Mach number of 2.0 and 1.5 respectively, have been tested, exploring a wide range of thermodynamic inlet conditions and diverse levels of non-ideality; from moderate non-ideal state, indicated by a compressibility factor Z = Pv/RT ≅ 0.80, to dilute gas conditions, Z ≥ 0.97. Maximum operating total pressure and temperature are PT ≅ 5 bar and TT ≅ 250 °C. The nozzle flow has been characterized in terms of total pressure, total temperature, static pressure at discrete locations along the nozzle axis, and schlieren imaging. In contrast to the well known case of polytropic ideal gas, the vapor expansion through the nozzle is found to be dependent on the inlet conditions, thus proving the non-ideal character of the flow. This influence is found to be consistent with the one predicted by the quasi-1D theory coupled with simple non-ideal gas models. Experimental data at the nozzle centerline have also been compared with those resulting from a two-dimensional viscous CFD calculation carried out using the SU2 software suite and the improved Peng Robinson Stryjek Vera (iPRSV) thermodynamic model. A very good accordance is found, demonstrating the high accuracy of the applied tools.

  • Numerical simulations of NICFD flows with SU2 vs experiments!

    Numerical simulations of NICFD flows with SU2 vs experiments!

    First-ever assessment of a CFD code against experimental data for non-ideal compressible-fluid flows of interests for ORC applications is ongoing. Grid adaptation helps capturing shock waves.

  • Wonderful time at NICFD in Varenna

    Wonderful time at NICFD in Varenna

    The 1st International Seminar on Non-Ideal Compressible-Fluid Dynamics was a great success!

    Thank you everyone for making this gathering so special.

  • Join us at NICFD 2016!

    Only two weeks to go before the 1st International Seminar on Non-Ideal Compressible-Fluid Dynamics for Propulsion & Power (NICFD 2016), the 20th and 21st of October, 2016, in Varenna, Como Lake, Italy

    Seminar website: nicfd2016.polimi.it                    Contact: nicfd2016@polimi.it
  • Laser Doppler Velocimetry @TROVA

    Laser Doppler Velocimetry @TROVA

    The first measurements using Laser Doppler Velocimetry are currently being carried out @TROVA. These are the first-ever velocity measurements within a non-ideal compressible-fluid flows in the close proximity of the liquid-vapour saturation curve. The flow seeding required the design and construction of a the pressurised seeding apparatus shown in the picture.

    Pressurised seeding system
    Laser source and photodetector.
    Note the (very cool!) laser safety goggles…
  • Seminar by Dr. Emile Touber, Imperial College

    Seminar by Dr. Emile Touber, Imperial College

    Shocks, turbulence and interactions in non-ideal and dense gases

    Dr. Emile Touber, Imperial College
    Abstract: Dense gases are characterised by molecules featuring large numbers of active degrees of freedom (quantified by the Cv/R ratio). The isentropes in such gases have the distinct property of following rather closely the isotherms (the two become identical in the limit of Cv/R going to infinity). Near the liquid-vapour critical point, this makes the isentropes very shallow and possibly concave (in the pressure-specific volume diagram). Whilst shallow isentropes are desirable when designing expanders (i.e. a large specific-volume increase may be achieved for virtually no pressure drop), could such extreme compressibility effects modify turbulence in a profound manner? This talk will discuss two particularly interesting aspects: (i) shock-refraction properties (i.e. the way a shock can redistribute the energy of incoming perturbations), (ii) the energy transfers in homogeneous turbulence (i.e. particularly the work done by the unsteady pressure force). In both cases we will show that non-convex isentropes are extremely influential in letting both the shock and the turbulence redistribute any supply of turbulence kinetic energy in ways which are simply not observable in ideal gases.
    March, the 17th, 2016 at 14:30 in Sala Consiglio Dipartimento di Scienze e Tecnologie Aerospaziali, Campus Bovisa La Masa, Via La Masa 34, 20156 Milano