Browsing by Author "Chiereghin, Nicola"

Browsing by Author "Chiereghin, Nicola"

Sort by: Order: Results:

  • MacManus, David G.; Chiereghin, Nicola; Gil-Prieto, Daniel; Zachos, Pavlos K. (AIAA, 2015-06-19)
    For many embedded and partially-embedded engine systems, the complexity of the flow field associated with convoluted intakes presents an area of notable research challenges. The convolution of the intake duct introduces ...
  • MacManus, David G.; Chiereghin, Nicola; Gil-Prieto, Daniel; Zachos, Pavlos K. (American Institute of Aeronautics and Astronautics, 2017-03-29)
    For many embedded engine systems, the intake duct geometry introduces flow distortion and unsteadiness, which must be understood when designing the turbomachinery components. The aim of this work is to investigate the ...
  • Gil-Prieto, Daniel; MacManus, David G.; Zachos, Pavlos K.; Tanguy, Geoffrey; Wilson, François; Chiereghin, Nicola (American Institute of Aeronautics and Astronautics, 2017-03-31)
    The dynamic flow distortion generated within convoluted aeroengine intakes can affect the performance and operability of the engine. There is a need for a better understanding of the main flow mechanisms that promote flow ...
  • Chiereghin, Nicola; MacManus, David G.; Savill, Mark; Dupuis, Romain (Royal Aeronautical Society (RAeS), 2015-07)
    This research focuses on the numerical simulation of the dynamic distortion in highly convoluted aeronautic intakes and extends the current knowledge with a systematic study of the influence of duct diameter, Mach number ...
  • Gil-Prieto, Daniel; MacManus, David G.; Zachos, Pavlos K.; Tanguy, Geoffrey; Wilson, Francois; Chiereghin, Nicola (American Institute of Aeronautics and Astronautics, 2016-06-30)
    The dynamic flow distortion generated within convoluted aero-engine intakes can affect the performance and operability of the engine. There is a need for a better understanding of the main flow mechanisms which promote ...
  • Zachos, Pavlos K.; MacManus, David G.; Chiereghin, Nicola (AIAA, 2015-06-19)
    The unsteady flow fields generated by convoluted aero engine intakes are major sources of instabilities that can compromise the performance of the down stream turbo machinery components. Hence, there exists a need for high ...
  • Zachos, Pavlos K.; MacManus, David G.; Chiereghin, Nicola (American Institute of Aeronautics and Astronautics, 2016-07-07)
    The unsteady flowfields generated by convoluted aero engine intakes are major sources of instabilities that can compromise the performance of the downstream turbomachinery components. Hence, there exists a need for high ...
  • Chiereghin, Nicola; Guglielmi, Luigi; Savill, Mark; Manca, Enrico; Rigobello, Aurora; Barison, Marco; Benini, Ernesto (AIAA, 2017-06-09)
    The Free Form Deformation method was applied to a S-duct geometry to reduce total pressure losses and flow distortion. The deformation method was coupled with a multiobjective genetic algorithm to optimize the shape of a ...