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Results: 1-13 |
Results: 13
WIND TURBINE PERFORMANCE UNDER ICING CONDITIONS
Authors: JASINSKI WJ NOE SC SELIG MS BRAGG MB
Citation: Wj. Jasinski et al., WIND TURBINE PERFORMANCE UNDER ICING CONDITIONS, Journal of solar energy engineering, 120(1), 1998, pp. 60-65
HYBRID AIRFOIL DESIGN METHOD TO SIMULATE FULL-SCALE ICE ACCRETION THROUGHOUT A GIVEN ALPHA-RANGE
Authors: SAEED F SELIG MS BRAGG MB
Citation: F. Saeed et al., HYBRID AIRFOIL DESIGN METHOD TO SIMULATE FULL-SCALE ICE ACCRETION THROUGHOUT A GIVEN ALPHA-RANGE, Journal of aircraft, 35(2), 1998, pp. 233-239
DESIGN OF SUBSCALE AIRFOILS WITH FULL-SCALE LEADING EDGES FOR ICE ACCRETION TESTING
Authors: SAEED F SELIG MS BRAGG MB
Citation: F. Saeed et al., DESIGN OF SUBSCALE AIRFOILS WITH FULL-SCALE LEADING EDGES FOR ICE ACCRETION TESTING, Journal of aircraft, 34(1), 1997, pp. 94-100
AIRFOIL BOUNDARY-LAYER DEVELOPMENT AND TRANSITION WITH LARGE LEADING-EDGE ROUGHNESS
Authors: KERHO ME BRAGG MB
Citation: Me. Kerho et Mb. Bragg, AIRFOIL BOUNDARY-LAYER DEVELOPMENT AND TRANSITION WITH LARGE LEADING-EDGE ROUGHNESS, AIAA journal, 35(1), 1997, pp. 75-84
BOUNDARY-LAYER-TRANSITION DUE TO ISOLATED 3-DIMENSIONAL ROUGHNESS ON AIRFOIL LEADING-EDGE
Authors: CUMMINGS MJ BRAGG MB
Citation: Mj. Cummings et Mb. Bragg, BOUNDARY-LAYER-TRANSITION DUE TO ISOLATED 3-DIMENSIONAL ROUGHNESS ON AIRFOIL LEADING-EDGE, AIAA journal, 34(9), 1996, pp. 1949-1952
FLOW OSCILLATION OVER AN AIRFOIL NEAR STALL
Authors: BRAGG MB HEINRICH DC BALOW FA ZAMAN KBMQ
Citation: Mb. Bragg et al., FLOW OSCILLATION OVER AN AIRFOIL NEAR STALL, AIAA journal, 34(1), 1996, pp. 199-201
AERODYNAMICS OF A FINITE WING WITH SIMULATED ICE
Authors: KHODADOUST A BRAGG MB
Citation: A. Khodadoust et Mb. Bragg, AERODYNAMICS OF A FINITE WING WITH SIMULATED ICE, Journal of aircraft, 32(1), 1995, pp. 137-144
STUDY OF THE DROPLET SPRAY CHARACTERISTICS OF A SUBSONIC WIND-TUNNEL
Authors: BRAGG MB KHODADOUST A
Citation: Mb. Bragg et A. Khodadoust, STUDY OF THE DROPLET SPRAY CHARACTERISTICS OF A SUBSONIC WIND-TUNNEL, Journal of aircraft, 32(1), 1995, pp. 199-204
NEUTRALLY BUOYANT BUBBLES USED AS FLOW TRACERS IN AIR
Authors: KERHO MF BRAGG MB
Citation: Mf. Kerho et Mb. Bragg, NEUTRALLY BUOYANT BUBBLES USED AS FLOW TRACERS IN AIR, Experiments in fluids, 16(6), 1994, pp. 393-400
EFFECT OF UNDERWING FROST ON A TRANSPORT AIRCRAFT AIRFOIL AT FLIGHT REYNOLDS-NUMBER
Authors: BRAGG MB HEINRICH DC VALAREZO WO MCGHEE RJ
Citation: Mb. Bragg et al., EFFECT OF UNDERWING FROST ON A TRANSPORT AIRCRAFT AIRFOIL AT FLIGHT REYNOLDS-NUMBER, Journal of aircraft, 31(6), 1994, pp. 1372-1379
EFFECT OF WIND-TUNNEL WALLS ON AIRFOIL DROPLET IMPINGEMENT
Authors: BRAGG MB WELLS SL
Citation: Mb. Bragg et Sl. Wells, EFFECT OF WIND-TUNNEL WALLS ON AIRFOIL DROPLET IMPINGEMENT, Journal of aircraft, 31(1), 1994, pp. 175-180
LOW-FREQUENCY FLOW OSCILLATION OVER AIRFOILS NEAR STALL
Authors: BRAGG MB HEINRICH DC KHODADOUST A
Citation: Mb. Bragg et al., LOW-FREQUENCY FLOW OSCILLATION OVER AIRFOILS NEAR STALL, AIAA journal, 31(7), 1993, pp. 1341-1343
EARLY VORTEX BURST ON A DELTA-WING IN PITCH
Authors: SOLTANI MR BRAGG MB
Citation: Mr. Soltani et Mb. Bragg, EARLY VORTEX BURST ON A DELTA-WING IN PITCH, AIAA journal, 31(12), 1993, pp. 2283-2289
Risultati: 1-13 |