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Results:
1-18
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Results: 18
Authors:
EKATERINARIS JA
Citation: Ja. Ekaterinaris, NUMERICAL-SIMULATION OF INCOMPRESSIBLE 2-BLADE ROTOR FLOWFIELDS, Journal of propulsion and power, 14(3), 1998, pp. 367-374
Authors:
EKATERINARIS JA
SORENSEN NN
RASMUSSEN F
Citation: Ja. Ekaterinaris et al., NUMERICAL INVESTIGATION OF AIRFOIL DYNAMIC STALL IN SIMULTANEOUS HARMONIC OSCILLATORY AND TRANSLATORY MOTION, Journal of solar energy engineering, 120(1), 1998, pp. 75-83
Authors:
EKATERINARIS JA
PLATZER MF
Citation: Ja. Ekaterinaris et Mf. Platzer, COMPUTATIONAL PREDICTION OF AIRFOIL DYNAMIC STALL, Progress in aerospace sciences, 33(11-12), 1997, pp. 759-846
Authors:
EKATERINARIS JA
Citation: Ja. Ekaterinaris, UPWIND SCHEME FOR ACOUSTIC DISTURBANCES GENERATED BY LOW-SPEED FLOWS, AIAA journal, 35(9), 1997, pp. 1448-1455
Authors:
EKATERINARIS JA
PLATZER MF
Citation: Ja. Ekaterinaris et Mf. Platzer, NUMERICAL INVESTIGATION OF STALL FLUTTER, Journal of turbomachinery, 118(2), 1996, pp. 197-203
Authors:
VANDYKEN RD
EKATERINARIS JA
CHANDRASEKHARA MS
PLATZER MF
Citation: Rd. Vandyken et al., ANALYSIS OF COMPRESSIBLE LIGHT DYNAMIC STALL FLOW AT TRANSITIONAL REYNOLDS-NUMBERS, AIAA journal, 34(7), 1996, pp. 1420-1427
Authors:
SRINIVASAN GR
EKATERINARIS JA
MCCROSKEY WJ
Citation: Gr. Srinivasan et al., EVALUATION OF TURBULENCE MODELS FOR UNSTEADY FLOWS OF AN OSCILLATING AIRFOIL, Computers & fluids, 24(7), 1995, pp. 833-861
Authors:
EKATERINARIS JA
Citation: Ja. Ekaterinaris, ANALYSIS OF FLOWFIELDS OVER MISSILE CONFIGURATIONS AT SUBSONIC SPEEDS, Journal of spacecraft and rockets, 32(3), 1995, pp. 385-391
Authors:
EKATERINARIS JA
COUTLEY RL
SCHIFF LB
PLATZER MF
Citation: Ja. Ekaterinaris et al., NUMERICAL INVESTIGATION OF HIGH-INCIDENCE FLOW OVER A DOUBLE-DELTA WING, Journal of aircraft, 32(3), 1995, pp. 457-463
Authors:
EKATERINARIS JA
CHANDRASEKHARA MS
PLATZER MF
Citation: Ja. Ekaterinaris et al., ANALYSIS OF LOW-REYNOLDS-NUMBER AIRFOIL FLOWS, Journal of aircraft, 32(3), 1995, pp. 625-630
Authors:
EKATERINARIS JA
SCHIFF LB
Citation: Ja. Ekaterinaris et Lb. Schiff, NAVIER-STOKES SOLUTION FOR AN OSCILLATING DOUBLE-DELTA WING, Journal of aircraft, 32(2), 1995, pp. 228-234
Authors:
EKATERINARIS JA
Citation: Ja. Ekaterinaris, NUMERICAL INVESTIGATION OF DYNAMIC STALL OF AN OSCILLATING WING, AIAA journal, 33(10), 1995, pp. 1803-1808
Authors:
TUNCER IH
EKATERINARIS JA
PLATZER MF
Citation: Ih. Tuncer et al., VISCOUS INVISCID INTERACTION METHOD FOR UNSTEADY LOW-SPEED AIRFOIL FLOWS, AIAA journal, 33(1), 1995, pp. 151-154
Authors:
EKATERINARIS JA
CRICELLI AS
PLATZER MF
Citation: Ja. Ekaterinaris et al., A ZONAL METHOD FOR UNSTEADY, VISCOUS, COMPRESSIBLE AIRFOIL FLOWS, Journal of fluids and structures, 8(1), 1994, pp. 107-123
Authors:
EKATERINARIS JA
SCHIFF LB
Citation: Ja. Ekaterinaris et Lb. Schiff, NUMERICAL-SIMULATION OF INCIDENCE AND SWEEP EFFECTS ON DELTA-WING VORTEX BREAKDOWN, Journal of aircraft, 31(5), 1994, pp. 1043-1049
Authors:
EKATERINARIS JA
MENTER FR
Citation: Ja. Ekaterinaris et Fr. Menter, COMPUTATION OF OSCILLATING AIRFOIL FLOWS WITH ONE-EQUATION AND 2-EQUATION TURBULENCE MODELS, AIAA journal, 32(12), 1994, pp. 2359-2365
Authors:
EKATERINARIS JA
Citation: Ja. Ekaterinaris, EFFECT OF SPATIAL ORDER OF ACCURACY ON THE COMPUTATION OF VORTICAL FLOWFIELDS, AIAA journal, 32(12), 1994, pp. 2471-2474
Authors:
EKATERINARIS JA
SCHIFF LB
Citation: Ja. Ekaterinaris et Lb. Schiff, NUMERICAL PREDICTION OF VORTICAL FLOW OVER SLENDER DELTA-WINGS, Journal of aircraft, 30(6), 1993, pp. 935-942
Risultati:
1-18
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