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Kenneth H. Yu
Kenneth H. Yu
University of Maryland, Department of Aerospace Engineering
Verified email at umd.edu - Homepage
Title
Cited by
Cited by
Year
Mixing enhancement in supersonic free shear flows
EJ Gutmark, KC Schadow, KH Yu
Annual Review of Fluid Mechanics 27 (1), 375-417, 1995
3661995
Low-frequency pressure oscillations in a model ramjet combustor
KH Yu, A Trouvé, JW Daily
Journal of Fluid Mechanics 232, 47-72, 1991
3611991
Combustion characteristics of boron nanoparticles
G Young, K Sullivan, MR Zachariah, K Yu
Combustion and flame 156 (2), 322-333, 2009
2772009
Effect of flame-holding cavities on supersonic-combustion performance
KH Yu, KJ Wilson, KC Schadow
Journal of Propulsion and Power 17 (6), 1287-1295, 2001
1632001
Cavity-actuated supersonic mixing and combustion control
KH Yu, KC Schadow
Combustion and Flame 99 (2), 295-301, 1994
1101994
Steady-State Analysis of Rotating Detonation Engine Flowfields with the Method of Characteristics
RT Fievisohn, KH Yu
Journal of Propulsion and Power 33 (1), 89-99, 2017
1022017
Analysis of the detonation wave structure in a linearized rotating detonation engine
S Prakash, R Fiévet, V Raman, J Burr, KH Yu
AIAA Journal, 1-15, 2019
782019
Shock Train/Boundary-Layer Interaction in Rectangular Isolators
JS Geerts, KH Yu
AIAA Journal 54 (11), 3450-3464, 2016
582016
Liquid-fueled active instability suppression
KH Yu, KJ Wilson, KC Schadow
Proceedings of the Combustion Institute 27 (2), 2039-2046, 1998
551998
Experimental investigation on dual-purpose cavity in supersonic reacting flows
K Yu, KJ Wilson, RA Smith, KC Schadow
36th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-98-0723, 1998
501998
Scale-up experiments on liquid-fueled active combustion control
KH Yu, KJ Wilson
Journal of propulsion and power 18 (1), 53-60, 2002
462002
Active control of liquid-fueled combustion using periodic vortex-droplet interaction
KH Yu, TP Parr, KJ Wilson, KC Schadow, EJ Gutmark
Proceedings of the Combustion Institute 26 (2), 2843-2850, 1996
461996
Combustion enhancement of a premixed flame by acoustic forcing with emphasis on role of large-scale vortical structures
K Yu, A Trouve, S Candel
29th AIAA Aerospace Sciences Meeting, AIAA-91-0367, 1991
441991
Experimental characterization of RDE combustor flowfield using linear channel
JR Burr, HY Ken
Proceedings of the Combustion Institute 37 (3), 3471-3478, 2019
392019
Method and device for modulation of a flame
KJ Wilson, KH Yu, T Parr, KC Schadow
US Patent 6,640,549, 2003
382003
Supersonic flow mixing and combustion using ramp nozzle
KH Yu, KC Schadow, KJ Kraeutle, EJ Gutmark
Journal of Propulsion and Power 11 (6), 1147-1153, 1995
381995
Focused Schlieren and Deflectometry at AEDC Hypervelocity Wind Tunnel No. 9
CP VanDercreek, MS Smith, KH Yu
40th AIAA Fluid Dynamics Conference, AIAA-2010-4209, 2010
372010
Investigation of supersonic mixing control using cavities: effect of fuel injection location
R Burnes, T Parr, K Wilson, K Yu
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA-2000-3618, 2000
352000
Detonation wave propagation in cross-flow of discretely spaced reactant jets
J Burr, KH Yu
53rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA-2017-4908, 2017
32*2017
Scramjet to ramjet transition in a dual-mode combustor with fin-guided injection
C Aguilera, KH Yu
Proceedings of the Combustion Institute 36 (2), 2911-2918, 2017
282017
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