Citation: Kw. Robinson et Jg. Leishman, EFFECTS OF BALLISTIC DAMAGE ON THE AERODYNAMICS OF HELICOPTER ROTOR AIRFOILS, Journal of aircraft, 35(5), 1998, pp. 695-703
Citation: E. Moedersheim et Jg. Leishman, INVESTIGATION OF AERODYNAMIC INTERACTIONS BETWEEN A ROTOR AND A T-TAIL EMPENNAGE, Journal of the American Helicopter Society, 43(1), 1998, pp. 37-46
Citation: A. Bagai et Jg. Leishman, ADAPTIVE-GRID SEQUENCING AND INTERPOLATION SCHEMES FOR HELICOPTER ROTOR WAKE ANALYSES, AIAA journal, 36(9), 1998, pp. 1593-1602
Citation: S. Winburn et al., ANGULAR RESPONSE PROPERTIES OF RETROREFLECTIVE SCREEN MATERIALS USED IN WIDE-FIELD SHADOWGRAPHY, Experiments in fluids, 20(3), 1996, pp. 227-229
Citation: N. Hariharan et Jg. Leishman, UNSTEADY AERODYNAMICS OF A FLAPPED AIRFOIL IN SUBSONIC FLOW BY INDICIAL CONCEPTS, Journal of aircraft, 33(5), 1996, pp. 855-868
Citation: Jg. Leishman et al., MEASUREMENTS OF ROTOR TIP VORTICES USING 3-COMPONENT LASER-DOPPLER VELOCIMETRY, Journal of the American Helicopter Society, 41(4), 1996, pp. 342-353
Citation: A. Bagai et Jg. Leishman, FREE-WAKE ANALYSIS OF TANDEM, TILT-ROTOR AND COAXIAL ROTOR CONFIGURATIONS, Journal of the American Helicopter Society, 41(3), 1996, pp. 196-207
Citation: A. Bagai et Jg. Leishman, ROTOR FREE-WAKE MODELING USING A PSEUDOIMPLICIT RELAXATION ALGORITHM, Journal of aircraft, 32(6), 1995, pp. 1276-1285
Citation: A. Bagai et Jg. Leishman, ROTOR FREE-WAKE MODELING USING A PSEUDO-IMPLICIT TECHNIQUE INCLUDING COMPARISONS WITH EXPERIMENTAL-DATA, Journal of the American Helicopter Society, 40(3), 1995, pp. 29-41
Citation: Jg. Leishman, UNSTEADY LIFT OF A FLAPPED AIRFOIL BY INDICIAL CONCEPTS (VOL 31, PG 288, 1994), Journal of aircraft, 31(5), 1994, pp. 1232-1232
Citation: Bg. Vanderwall et Jg. Leishman, ON THE INFLUENCE OF TIME-VARYING FLOW VELOCITY ON UNSTEADY AERODYNAMICS, Journal of the American Helicopter Society, 39(4), 1994, pp. 25-36
Citation: A. Bagai et Jg. Leishman, FLOW VISUALIZATION OF COMPRESSIBLE VORTEX STRUCTURES USING DENSITY GRADIENT TECHNIQUES, Experiments in fluids, 15(6), 1993, pp. 431-442
Citation: Jg. Leishman, INDICIAL LIFT APPROXIMATIONS FOR 2-DIMENSIONAL SUBSONIC FLOW AS OBTAINED FROM OSCILLATORY MEASUREMENTS, Journal of aircraft, 30(3), 1993, pp. 340-351
Citation: A. Zandieh et Jg. Leishman, BOUNDARY-LAYER AND PRESSURE MEASUREMENTS ON A CYLINDER WITH UNSTEADY CIRCULATION CONTROL, AIAA journal, 31(10), 1993, pp. 1769-1776