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Erinc Erdem
Erinc Erdem
TUSAS Engine Industries
Verified email at tei.com.tr - Homepage
Title
Cited by
Cited by
Year
Numerical and experimental investigation of transverse injection flows
E Erdem, K Kontis
Shock Waves 20, 103-118, 2010
1492010
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
862014
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
562014
Steady energy deposition at Mach 5 for drag reduction
E Erdem, K Kontis, L Yang
Shock Waves 23 (4), 285-298, 2013
532013
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
512012
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
442012
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
382013
Experimental investigation of sonic transverse jets in Mach 5 crossflow
E Erdem, K Kontis
Aerospace Science and Technology 110, 106419, 2021
322021
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
322014
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
322012
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
262011
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
232009
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
192006
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
172012
Active flow control studies at Mach 5: measurement and computation
E Erdem
The University of Manchester, Manchester, UK, 2011
172011
Thrust vector control by secondary injection
E Erdem
Middle East Technical University, 2006
162006
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
112009
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
102012
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
102010
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
92008
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