Bibliography
301
Wind Tunnels of the ONERA Lille Centre
Atinault O, Carrier G, Grenon R, Verbeke C, Viscat P (2013) Numerical and experimental aerodynamic investigations of boundary layer ingestion for improving propulsion efficiency of future
air transport. In: 31st AIAA applied aerodynamics conference, San Diego, 24–27 June 2013
Mouton S, Rantet E, Gouverneur G, Verbeke C (2012) Combined wind tunnel tests and flow simulations for light aircraft performance prediction. In: 3AF 47th symposium of applied aerodynamics,
Paris, 26–28 Mar 2012
Pape AL, Lienard C, Verbeke C, Pruvost M, De Coninck JL (2003) Helicopter fuselage drag
reduction using active flow control: a comprehensive experimental investigation. J Am Helicopter
Soc 60(3):1
Verbeke C, Mialon B (2014) Naval aerodynamics: State of the art measurement and computational
techniques. In: 3AF 49th international symposium of applied aerodynamics, Lille, France, 24–26
Mar 2014
Verbeke C, Eglinger E, Atinault O, Grenon R, Carrier G, Mialon B, Ternoy F (2014) Experimental investigation of the boundary layer ingestion: specificity and challenges. In: 3AF 49th
international symposium of applied aerodynamics, Lille, France, 24–26 Mar 2014
World-Directory (1990) World directory of aerospace vehicle research and development. WorldDirectory, Washington, DC
Wind Tunnels of the Institut de Mécanique des Fluides de
Toulouse
Deri E, Braza M, Cazin S, Cid E, Degouet C, Michaelis D (2014) Investigation of the threedimensional turbulent near-wake structure past a flat plate by tomographic PIV at high Reynolds
number. J Fluids Struct 47:21–30
Mockett C, Perrin R, Reimann T, Braza M, Thiele F (2010) Analysis of detached-eddy simulation for
the flow around a circular cylinder with reference to PIV data. J Flow, Turb Combust 85(2):167–
180
Perrin R, Braza M, Cid E, Cazin S, Chassaing P, Mockett C, Reimann T, Thiele F (2008) Coherent
and turbulent process analysis in the flow past a circular cylinder at high Reynolds number. J
Fluids Struct 24(8):1313–1325
Scheller J, Chinaud M, Rouchon JF, Duhayon E, Cazin S, Marchal M, Braza M (2015) Trailing-edge
dynamics of a morphing NACA0012 aileron at high Reynolds number by time-resolved PIV. J
Fluids Struct 55:42–51
The CIRA Icing Wind Tunnel
Bellucci M, Esposito BM, Marrazzo M, Esposito B, Ferrigno F (2007) Calibration of the CIRA
IWT in low speed configuration. In: 45th AIAA aerospace sciences meeting and exhibit, Reno,
Nevada, AIAA-2007-1092, 8–11 Jan 2007
Esposito BM, Ragni A, Ferrigno F, Vecchione L (2003) Update on the icing cloud calibration of
the CIRA Icing Wind Tunnel. SAE 2003 Transactions, J Aerosp, vol 112, Sec 1, p 47, Apr 2003
Oleskiw MM, Esposito BM, de Gregorio F (1996) The effect of altitude on icing tunnel airfoil
icing simulation. In: Proceedings of the FAA international conference on aircraft inflight icing,
DOT/FAA/AR-96/81, II, pp 511–520, Aug 1996
301
Wind Tunnels of the ONERA Lille Centre
Atinault O, Carrier G, Grenon R, Verbeke C, Viscat P (2013) Numerical and experimental aerodynamic investigations of boundary layer ingestion for improving propulsion efficiency of future
air transport. In: 31st AIAA applied aerodynamics conference, San Diego, 24–27 June 2013
Mouton S, Rantet E, Gouverneur G, Verbeke C (2012) Combined wind tunnel tests and flow simulations for light aircraft performance prediction. In: 3AF 47th symposium of applied aerodynamics,
Paris, 26–28 Mar 2012
Pape AL, Lienard C, Verbeke C, Pruvost M, De Coninck JL (2003) Helicopter fuselage drag
reduction using active flow control: a comprehensive experimental investigation. J Am Helicopter
Soc 60(3):1
Verbeke C, Mialon B (2014) Naval aerodynamics: State of the art measurement and computational
techniques. In: 3AF 49th international symposium of applied aerodynamics, Lille, France, 24–26
Mar 2014
Verbeke C, Eglinger E, Atinault O, Grenon R, Carrier G, Mialon B, Ternoy F (2014) Experimental investigation of the boundary layer ingestion: specificity and challenges. In: 3AF 49th
international symposium of applied aerodynamics, Lille, France, 24–26 Mar 2014
World-Directory (1990) World directory of aerospace vehicle research and development. WorldDirectory, Washington, DC
Wind Tunnels of the Institut de Mécanique des Fluides de
Toulouse
Deri E, Braza M, Cazin S, Cid E, Degouet C, Michaelis D (2014) Investigation of the threedimensional turbulent near-wake structure past a flat plate by tomographic PIV at high Reynolds
number. J Fluids Struct 47:21–30
Mockett C, Perrin R, Reimann T, Braza M, Thiele F (2010) Analysis of detached-eddy simulation for
the flow around a circular cylinder with reference to PIV data. J Flow, Turb Combust 85(2):167–
180
Perrin R, Braza M, Cid E, Cazin S, Chassaing P, Mockett C, Reimann T, Thiele F (2008) Coherent
and turbulent process analysis in the flow past a circular cylinder at high Reynolds number. J
Fluids Struct 24(8):1313–1325
Scheller J, Chinaud M, Rouchon JF, Duhayon E, Cazin S, Marchal M, Braza M (2015) Trailing-edge
dynamics of a morphing NACA0012 aileron at high Reynolds number by time-resolved PIV. J
Fluids Struct 55:42–51
The CIRA Icing Wind Tunnel
Bellucci M, Esposito BM, Marrazzo M, Esposito B, Ferrigno F (2007) Calibration of the CIRA
IWT in low speed configuration. In: 45th AIAA aerospace sciences meeting and exhibit, Reno,
Nevada, AIAA-2007-1092, 8–11 Jan 2007
Esposito BM, Ragni A, Ferrigno F, Vecchione L (2003) Update on the icing cloud calibration of
the CIRA Icing Wind Tunnel. SAE 2003 Transactions, J Aerosp, vol 112, Sec 1, p 47, Apr 2003
Oleskiw MM, Esposito BM, de Gregorio F (1996) The effect of altitude on icing tunnel airfoil
icing simulation. In: Proceedings of the FAA international conference on aircraft inflight icing,
DOT/FAA/AR-96/81, II, pp 511–520, Aug 1996