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Results:
1-10
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Results: 10
Authors:
AVITAL EJ
SANDHAM ND
LUO KH
Citation: Ej. Avital et al., MACH WAVE RADIATION BY MIXING LAYERS - PART I - ANALYSIS OF THE SOUNDFIELD, Theoretical and computational fluid dynamics, 12(2), 1998, pp. 73-90
Authors:
AVITAL EJ
SANDHAM ND
LUO KH
Citation: Ej. Avital et al., MACH WAVE RADIATION BY MIXING LAYERS - PART II - ANALYSIS OF THE SOURCE FIELD, Theoretical and computational fluid dynamics, 12(2), 1998, pp. 91-108
Authors:
LUO KH
SANDHAM ND
Citation: Kh. Luo et Nd. Sandham, INSTABILITY OF VORTICAL AND ACOUSTIC MODES IN SUPERSONIC ROUND JETS, Physics of fluids, 9(4), 1997, pp. 1003-1013
Authors:
AVITAL EJ
SANDHAM ND
Citation: Ej. Avital et Nd. Sandham, A NOTE ON THE STRUCTURE OF THE ACOUSTIC FIELD EMITTED BY A WAVE-PACKET, Journal of sound and vibration, 204(3), 1997, pp. 533-539
Authors:
LUO KH
SANDHAM ND
Citation: Kh. Luo et Nd. Sandham, DIRECT NUMERICAL-SIMULATION OF SUPERSONIC JET FLOW, Journal of engineering mathematics, 32(2-3), 1997, pp. 121-142
Authors:
AVITAL EJ
SANDHAM ND
Citation: Ej. Avital et Nd. Sandham, BOX-LENGTH REQUIREMENTS FOR SIMULATION OF SOUND FROM LARGE STRUCTURESIN JETS, AIAA journal, 35(5), 1997, pp. 912-915
Authors:
VREMAN AW
SANDHAM ND
LUO KH
Citation: Aw. Vreman et al., COMPRESSIBLE MIXING LAYER GROWTH-RATE AND TURBULENCE CHARACTERISTICS, Journal of Fluid Mechanics, 320, 1996, pp. 235-258
Authors:
SANDHAM ND
ADAMS NA
KLEISER L
Citation: Nd. Sandham et al., DIRECT SIMULATION OF BREAKDOWN TO TURBULENCE FOLLOWING OBLIQUE INSTABILITY WAVES IN A SUPERSONIC BOUNDARY-LAYER, Applied scientific research, 54(3), 1995, pp. 223-234
Authors:
SANDHAM ND
Citation: Nd. Sandham, THE EFFECT OF COMPRESSIBILITY ON VORTEX PAIRING, Physics of fluids, 6(2), 1994, pp. 1063-1072
Authors:
SANDHAM ND
ADAMS NA
Citation: Nd. Sandham et Na. Adams, NUMERICAL-SIMULATION OF BOUNDARY-LAYER-TRANSITION AT MACH 2, Applied scientific research, 51(1-2), 1993, pp. 371-375
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