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Gorchakova N, Kuznetsov L, Yarygin V, Chanetz B, Pot T, Bur R, Taran JP, Pigache D, Schulte D,
Moss J (2002) Progress in shock wave/boundary layer interactions studies in rarefied hypersonic
flows using electron beam excited X-ray detection. AIAA J
Gross KP, Mc Kenzie RL, Logan P (1987) Measurements of temperature, density, pressure, and their
fluctuations in supersonic turbulence using laser-induced fluorescence. Exp Fluids 5:372–380
Hiller B, Hanson RK (1988) Simultaneous planar measurements of velocity and pressure fields in
gas flows using laser-induced fluorescence. Appl Opt 27(1):33–48
Kuznetsov L, Rebrov A, Yarigin V (1973) Diagnostics of ionized gas by electron beam in X-ray
spectrum range. In: 11th international conference on phenomena in ionized gases, Prague
Larigaldie S, Bize D, Mohamed AK, Ory M, Soutadé J, Taran JP (1998) Velocity measurement
in high enthalpy, hypersonic flows using an electron beam assisted glow discharge. AIAA J
36(6):1061
Lefebvre M, Chanetz B, Pot T, Bouchardy P, Varghese P (1994) Measurement by coherent anti-sokes
Raman Scattering in the R5Ch hypersonic wind tunnel. Aerosp Res (4):295–298
Mohamed AK, Pot T, Chanetz B (1995) Diagnostics by electron beam florescence in hypersonics.
In: 16th international congress on instrumentation in aerospace facilities, Dayton, OH, 18–21
July 1995
Chapter 13: Computer-Aided Wind Tunnel and Analysis
Esteve MJ, Esteve N (2012) CFD/WTT synergy towards an enhanced A/C performance prediction
at Airbus. In: 3AF 47th international conference on applied aerodynamics, Paris, 26–28 Mar 2012
Foures DPG, Dovetta N, Sipp D, Schmid PJ (2014) A data-assimilation method for Reynoldsaveraged Navier-Stokes-driven mean flow reconstruction. J Fluid Mech 759:404–431
Hantrais-Gervois JL, Piat JF (2012) A methodology to derive wind tunnel wall corrections from
RANS simulations. In: 5th symposium on integrating CFD and experiments in aerodynamics
(integration 2012), JAXA Chofu Aerospace Center, Tokyo, Japan, 3–5 Oct 2012
Watanabe S, Kuchi-Ishi S, Murakami K, Hashimoto A, Kato H, Yamashita T, Yasue K, Imagawa
K, Nakakita K (2012) Development status of a prototype system for EFD/CFD integration. In:
3AF 47th international conference on applied aerodynamics, Paris, 26–28 Mar 2012
Chapter 14: Prospects and Challenges for Aerodynamics
Arnal D (2008) Practical transition prediction methods: Subsonic and transonic flows. VKI lecture
series advances in laminar-turbulent transition modelling
Marchiano R, Druault P, Leiba R, Marchal J, Ollivier F, Valeau V. et Vanwynsberghe C (2016) Localisation de sources aéroacoustiques par une méthode de retournement temporel tridimensionnelle.
In: 13ème Congrès Français d’Acoustique, Le Mans, pp 1899–1905 [N°000353], 11–15 Avril
2016
Van Herpe F, Totaro N, Lafont T, Lazure H, et Laumonier J (2016) Prédiction de bruit d’origine
aérodynamique en moyennes fréquences par la méthode SmEdA. In: 13ème Congrès Francais
d’Acoustique, Le Mans, pp 1453–1459 [N°000374], 11–15 Avril 2016
Vermeersch O, Yoshida K, Ueda Y, Arnal D (2012) Transition prediction on a supersonic natural laminar flow wing: experiments and computations. In: 3AF 47th conference on applied
aerodynamics, Paris, 26–28 Mar 2012
309
Gorchakova N, Kuznetsov L, Yarygin V, Chanetz B, Pot T, Bur R, Taran JP, Pigache D, Schulte D,
Moss J (2002) Progress in shock wave/boundary layer interactions studies in rarefied hypersonic
flows using electron beam excited X-ray detection. AIAA J
Gross KP, Mc Kenzie RL, Logan P (1987) Measurements of temperature, density, pressure, and their
fluctuations in supersonic turbulence using laser-induced fluorescence. Exp Fluids 5:372–380
Hiller B, Hanson RK (1988) Simultaneous planar measurements of velocity and pressure fields in
gas flows using laser-induced fluorescence. Appl Opt 27(1):33–48
Kuznetsov L, Rebrov A, Yarigin V (1973) Diagnostics of ionized gas by electron beam in X-ray
spectrum range. In: 11th international conference on phenomena in ionized gases, Prague
Larigaldie S, Bize D, Mohamed AK, Ory M, Soutadé J, Taran JP (1998) Velocity measurement
in high enthalpy, hypersonic flows using an electron beam assisted glow discharge. AIAA J
36(6):1061
Lefebvre M, Chanetz B, Pot T, Bouchardy P, Varghese P (1994) Measurement by coherent anti-sokes
Raman Scattering in the R5Ch hypersonic wind tunnel. Aerosp Res (4):295–298
Mohamed AK, Pot T, Chanetz B (1995) Diagnostics by electron beam florescence in hypersonics.
In: 16th international congress on instrumentation in aerospace facilities, Dayton, OH, 18–21
July 1995
Chapter 13: Computer-Aided Wind Tunnel and Analysis
Esteve MJ, Esteve N (2012) CFD/WTT synergy towards an enhanced A/C performance prediction
at Airbus. In: 3AF 47th international conference on applied aerodynamics, Paris, 26–28 Mar 2012
Foures DPG, Dovetta N, Sipp D, Schmid PJ (2014) A data-assimilation method for Reynoldsaveraged Navier-Stokes-driven mean flow reconstruction. J Fluid Mech 759:404–431
Hantrais-Gervois JL, Piat JF (2012) A methodology to derive wind tunnel wall corrections from
RANS simulations. In: 5th symposium on integrating CFD and experiments in aerodynamics
(integration 2012), JAXA Chofu Aerospace Center, Tokyo, Japan, 3–5 Oct 2012
Watanabe S, Kuchi-Ishi S, Murakami K, Hashimoto A, Kato H, Yamashita T, Yasue K, Imagawa
K, Nakakita K (2012) Development status of a prototype system for EFD/CFD integration. In:
3AF 47th international conference on applied aerodynamics, Paris, 26–28 Mar 2012
Chapter 14: Prospects and Challenges for Aerodynamics
Arnal D (2008) Practical transition prediction methods: Subsonic and transonic flows. VKI lecture
series advances in laminar-turbulent transition modelling
Marchiano R, Druault P, Leiba R, Marchal J, Ollivier F, Valeau V. et Vanwynsberghe C (2016) Localisation de sources aéroacoustiques par une méthode de retournement temporel tridimensionnelle.
In: 13ème Congrès Français d’Acoustique, Le Mans, pp 1899–1905 [N°000353], 11–15 Avril
2016
Van Herpe F, Totaro N, Lafont T, Lazure H, et Laumonier J (2016) Prédiction de bruit d’origine
aérodynamique en moyennes fréquences par la méthode SmEdA. In: 13ème Congrès Francais
d’Acoustique, Le Mans, pp 1453–1459 [N°000374], 11–15 Avril 2016
Vermeersch O, Yoshida K, Ueda Y, Arnal D (2012) Transition prediction on a supersonic natural laminar flow wing: experiments and computations. In: 3AF 47th conference on applied
aerodynamics, Paris, 26–28 Mar 2012
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