Arvind Gangoli Rao
Arvind Gangoli Rao
Professor, Sustainable Aircraft Propulsion, Delft University of Technology
Verified email at - Homepage
Cited by
Cited by
Infrared signature studies of aerospace vehicles
SP Mahulikar, HR Sonawane, GA Rao
Progress in aerospace sciences 43 (7-8), 218-245, 2007
Integrated review of stealth technology and its role in airpower
GA Rao, SP Mahulikar
The aeronautical journal 106 (1066), 629-642, 2002
Flameless combustion and its potential towards gas turbines
AAV Perpignan, AG Rao, DJEM Roekaerts
Progress in Energy and Combustion Science 69, 28-62, 2018
New criterion for aircraft susceptibility to infrared guided missiles
GA Rao, SP Mahulikar
Aerospace science and technology 9 (8), 701-712, 2005
Effect of atmospheric transmission and radiance on aircraft infared signatures
GA Rao, SP Mahulikar
Journal of aircraft 42 (4), 1046-1054, 2005
Analysis and design of hybrid electric regional turboprop aircraft
M Voskuijl, J Van Bogaert, AG Rao
CEAS Aeronautical Journal 9 (1), 15-25, 2018
Infrared signatures of low-flying aircraft and their rear fuselage skin's emissivity optimization
SP Mahulikar, GA Rao, PS Kolhe
Journal of Aircraft 43 (1), 226-232, 2006
Numerical investigations of heat transfer and pressure drop characteristics in multiple jet impingement system
PS Penumadu, AG Rao
Applied Thermal Engineering 110, 1511-1524, 2017
Aircraft powerplant and plume infrared signature modelling and analysis
AG Rao
43 rd AIAA Aerospace Sciences Meeting and Exhibit, 2005, 2005
Aircraft plume infrared signature in nonafterburning mode
SP Mahulikar, GA Rao, SK Sane, AG Marathe
Journal of thermophysics and heat transfer 19 (3), 413-415, 2005
Study of sunshine, skyshine, and earthshine for aircraft infrared detection
SP Mahulikar, SK Potnuru, GA Rao
Journal of Optics A: Pure and Applied Optics 11 (4), 045703, 2009
A hybrid engine concept for multi-fuel blended wing body
AG Rao, F Yin, JP van Buijtenen
Aircraft Engineering and Aerospace Technology: An International Journal, 2014
Skin-temperature prediction of aircraft rear fuselage with multimode thermal model
SP Mahulikar, PS Kolhe, GA Rao
Journal of Thermophysics and Heat Transfer 19 (1), 114-124, 2005
Investigation of flow characteristics in lean direct injection combustors
D Dewanji, AG Rao, M Pourquie, JP Van Buijtenen
Journal of Propulsion and Power 28 (1), 181-196, 2012
A new combustion methodology for low emission gas turbine engines
AG Rao, Y Levy
8th HiTACG conference, Poznan, 13, 2010
Numerical analysis of a multiple jet impingement system
GA Rao, M Kitron-Belinkov, Y Levy
Turbo Expo: Power for Land, Sea, and Air 48845, 629-639, 2009
Emission modeling of an interturbine burner based on flameless combustion
AAV Perpignan, MG Talboom, Y Levy, AG Rao
Energy & Fuels 32 (1), 822-838, 2018
Performance assessment of a multi-fuel hybrid engine for future aircraft
F Yin, AG Rao, A Bhat, M Chen
Aerospace Science and Technology 77, 217-227, 2018
Assessing the climate impact of the AHEAD multi-fuel blended wing body
V Grewe, L Bock, U Burkhardt, K Dahlmann, KM Gierens, L Hüttenhofer, ...
Meteorologische Zeitschrift 26 (6), 711-725, 2017
Performance analysis of an electrically assisted propulsion system for a short-range civil aircraft
AWX Ang, A Gangoli Rao, T Kanakis, W Lammen
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2019
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