Numerical and experimental investigation of transverse injection flows E Erdem, K Kontis Shock Waves 20, 103-118, 2010 | 149 | 2010 |
Effectiveness of jet location on mixing characteristics inside a cavity in supersonic flow T Ukai, H Zare-Behtash, E Erdem, KH Lo, K Kontis, S Obayashi Experimental thermal and fluid science 52, 59-67, 2014 | 86 | 2014 |
Laser energy deposition effectiveness on shock-wave boundary-layer interactions over cylinder-flare combinations T Osuka, E Erdem, N Hasegawa, R Majima, T Tamba, S Yokota, A Sasoh, ... Physics of Fluids 26 (9), 2014 | 56 | 2014 |
Steady energy deposition at Mach 5 for drag reduction E Erdem, K Kontis, L Yang Shock Waves 23 (4), 285-298, 2013 | 53 | 2013 |
Investigation of the double ramp in hypersonic flow using luminescent measurement systems L Yang, H Zare-Behtash, E Erdem, K Kontis Experimental thermal and fluid science 40, 50-56, 2012 | 51 | 2012 |
Application of AA-PSP to hypersonic flows: The double ramp model L Yang, H Zare-Behtash, E Erdem, K Kontis Sensors and Actuators B: Chemical 161 (1), 100-107, 2012 | 44 | 2012 |
Experiments on transitional shock wave--boundary layer interactions at Mach 5 E Erdem, K Kontis, E Johnstone, NP Murray, J Steelant Experiments in fluids 54, 1-22, 2013 | 39 | 2013 |
Experimental investigation of sonic transverse jets in Mach 5 crossflow E Erdem, K Kontis Aerospace Science and Technology 110, 106419, 2021 | 32 | 2021 |
Penetration characteristics of air, carbon dioxide and helium transverse sonic jets in mach 5 cross flow E Erdem, K Kontis, S Saravanan Sensors 14 (12), 23462-23489, 2014 | 32 | 2014 |
Pressure-sensitive paint on a truncated cone in hypersonic flow at incidences L Yang, E Erdem, H Zare-Behtash, K Kontis, S Saravanan International journal of heat and fluid flow 37, 9-21, 2012 | 32 | 2012 |
Drag reduction studies by steady energy deposition at Mach 5 E Erdem, L Yang, K Kontis 49th AIAA aerospace sciences meeting including the new horizons forum and …, 2011 | 26 | 2011 |
Drag reduction by energy deposition in hypersonic flows E Erdem, L Yang, K Kontis 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and …, 2009 | 23 | 2009 |
Parametric study of secondary gas injection into a conical rocket nozzle for thrust vectoring E Erdem, K Albayrak, T Tinaztepe 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4942, 2006 | 19 | 2006 |
Experimental investigation of transverse injection flowfield at march 5 and the influence of impinging shock wave E Erdem, S Saravanan, J Lin, K Kontis 18th AIAA/3AF International Space Planes and Hypersonic Systems and …, 2012 | 17 | 2012 |
Active flow control studies at Mach 5: measurement and computation E Erdem The University of Manchester, Manchester, UK, 2011 | 17 | 2011 |
Thrust vector control by secondary injection E Erdem Middle East Technical University, 2006 | 16 | 2006 |
Non-plasma and plasma transverse jets in hypersonic cross flow E Erdem, K Kontis 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and …, 2009 | 11 | 2009 |
Experimental Studies on Micro-ramps at Mach 5 R Saad, E Erdem, L Yang, K Kontis 28th International Symposium on Shock Waves: Vol 2, 861-866, 2012 | 10 | 2012 |
Flow control using thermal bumps in hypersonic flows L Yang, E Erdem, K Kontis 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010 | 10 | 2010 |
Numerical investigation of flowfield inside a conical rocket nozzle in the presence of transverse injection E Erdem, K Kontis, K Albayrak, T Tinaztepe 46th AIAA Aerospace Sciences Meeting and Exhibit, 359, 2008 | 9 | 2008 |