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Results: 1-18 |
Results: 18
DETERMINING THE FREQUENCY OF BREAST IMPLANT FAILURE REQUIRES SOUND SCIENTIFIC PRINCIPLES
Authors: YOUNG VL PETERS W BRANDON HJ JERINA KL WOLF CJ
Citation: Vl. Young et al., DETERMINING THE FREQUENCY OF BREAST IMPLANT FAILURE REQUIRES SOUND SCIENTIFIC PRINCIPLES, Plastic and reconstructive surgery, 102(4), 1998, pp. 1295-1299
MICROSTRUCTURAL DIFFERENCES BETWEEN WOVEN MAT AND ACRYLIC BINDER TMC AND THEIR RELATIONSHIP TO FATIGUE DAMAGE MODES
Authors: HARMON D JERINA KL SASTRY SML
Citation: D. Harmon et al., MICROSTRUCTURAL DIFFERENCES BETWEEN WOVEN MAT AND ACRYLIC BINDER TMC AND THEIR RELATIONSHIP TO FATIGUE DAMAGE MODES, Journal of composite materials, 31(15), 1997, pp. 1534-1554
DEFORMATION-BEHAVIOR OF A RAPIDLY SOLIDIFIED FINE-GRAINED AL-8.5-PERCENT-FE-1.2-PERCENT-V-1.7-PERCENT-SI ALLOY
Authors: HARIPRASAD S SASTRY SML JERINA KL
Citation: S. Hariprasad et al., DEFORMATION-BEHAVIOR OF A RAPIDLY SOLIDIFIED FINE-GRAINED AL-8.5-PERCENT-FE-1.2-PERCENT-V-1.7-PERCENT-SI ALLOY, Acta materialia, 44(1), 1996, pp. 383-389
UNDERCOOLING AND SUPERSATURATION OF ALLOYING ELEMENTS IN RAPIDLY SOLIDIFIED AL-8.5-PERCENT FE-1.2-PERCENT V-1.7-PERCENT SI ALLOY
Authors: HARIPRASAD S SASTRY SML JERINA KL
Citation: S. Hariprasad et al., UNDERCOOLING AND SUPERSATURATION OF ALLOYING ELEMENTS IN RAPIDLY SOLIDIFIED AL-8.5-PERCENT FE-1.2-PERCENT V-1.7-PERCENT SI ALLOY, Journal of Materials Science, 31(4), 1996, pp. 921-925
CREEP-FATIGUE LIFE PREDICTION OF IN-SITU COMPOSITE SOLDERS
Authors: KUO CG SASTRY SML JERINA KL
Citation: Cg. Kuo et al., CREEP-FATIGUE LIFE PREDICTION OF IN-SITU COMPOSITE SOLDERS, Metallurgical and materials transactions. A, Physical metallurgy andmaterials science, 26(12), 1995, pp. 3265-3275
THE EFFECT OF ALLOYING ADDITIONS ON THE HIGH-TEMPERATURE DEFORMATION CHARACTERISTICS OF TI-48AL (AT-PERCENT) ALLOYS
Authors: SABINASH CM SASTRY SML JERINA KL
Citation: Cm. Sabinash et al., THE EFFECT OF ALLOYING ADDITIONS ON THE HIGH-TEMPERATURE DEFORMATION CHARACTERISTICS OF TI-48AL (AT-PERCENT) ALLOYS, Scripta metallurgica et materialia, 32(9), 1995, pp. 1381-1386
HIGH-TEMPERATURE DEFORMATION OF TITANIUM ALUMINIDE ALLOYS
Authors: SABINASH CM SASTRY SML JERINA KL
Citation: Cm. Sabinash et al., HIGH-TEMPERATURE DEFORMATION OF TITANIUM ALUMINIDE ALLOYS, Materials science & engineering. A, Structural materials: properties, microstructure and processing, 193, 1995, pp. 837-847
CONSOLIDATION AND MECHANICAL-PROPERTIES OF MOSI2-BASED MATERIALS
Authors: SASTRY SML SURYANARAYANAN R JERINA KL
Citation: Sml. Sastry et al., CONSOLIDATION AND MECHANICAL-PROPERTIES OF MOSI2-BASED MATERIALS, Materials science & engineering. A, Structural materials: properties, microstructure and processing, 193, 1995, pp. 881-890
FATIGUE-CRACK GROWTH-RATES AND FRACTURE-TOUGHNESS OF RAPIDLY SOLIDIFIED AL-8.5 PCT FE-1.2 PCT V-1.7 PCT SI ALLOYS
Authors: HARIPRASAD S SASTRY SML JERINA KL LEDERICH RJ
Citation: S. Hariprasad et al., FATIGUE-CRACK GROWTH-RATES AND FRACTURE-TOUGHNESS OF RAPIDLY SOLIDIFIED AL-8.5 PCT FE-1.2 PCT V-1.7 PCT SI ALLOYS, Metallurgical and materials transactions. A, Physical metallurgy andmaterials science, 25(5), 1994, pp. 1005-1014
THE EFFECT OF POROSITY ON ELASTIC-CONSTANTS OF REPRESENTATIVE AIRCRAFT LAMINATES
Authors: RUBIN AM JERINA KL
Citation: Am. Rubin et Kl. Jerina, THE EFFECT OF POROSITY ON ELASTIC-CONSTANTS OF REPRESENTATIVE AIRCRAFT LAMINATES, Journal of advanced materials, 25(4), 1994, pp. 21-30
HIGH-TEMPERATURE DEFORMATION CHARACTERISTICS OF TI(41-52) AT-PERCENT AL-ALLOYS
Authors: SABINASH CM SASTRY SML JERINA KL
Citation: Cm. Sabinash et al., HIGH-TEMPERATURE DEFORMATION CHARACTERISTICS OF TI(41-52) AT-PERCENT AL-ALLOYS, Scripta metallurgica et materialia, 30(11), 1994, pp. 1391-1396
CONSOLIDATION OF MOLYBDENUM DISILICIDE BASED MATERIALS BY HOT ISOSTATIC PRESSING (HIP) - COMPARISON WITH MODELS
Authors: SURYANARAYANAN R SASTRY SML JERINA KL
Citation: R. Suryanarayanan et al., CONSOLIDATION OF MOLYBDENUM DISILICIDE BASED MATERIALS BY HOT ISOSTATIC PRESSING (HIP) - COMPARISON WITH MODELS, Acta metallurgica et materialia, 42(11), 1994, pp. 3741-3750
MECHANICAL-PROPERTIES OF MOLYBDENUM DISILICIDE BASED MATERIALS CONSOLIDATED BY HOT ISOSTATIC PRESSING (HIP)
Authors: SURYANARAYANAN R SASTRY SML JERINA KL
Citation: R. Suryanarayanan et al., MECHANICAL-PROPERTIES OF MOLYBDENUM DISILICIDE BASED MATERIALS CONSOLIDATED BY HOT ISOSTATIC PRESSING (HIP), Acta metallurgica et materialia, 42(11), 1994, pp. 3751-3757
ROOM-TEMPERATURE TENSILE PROPERTIES OF SN-5-PERCENT-SB SOLDER
Authors: MAHIDHARA RK SASTRY SML JERINA KL TURLIK I MURTY KL
Citation: Rk. Mahidhara et al., ROOM-TEMPERATURE TENSILE PROPERTIES OF SN-5-PERCENT-SB SOLDER, Journal of materials science letters, 13(19), 1994, pp. 1387-1389
EVALUATION OF POROSITY IN COMPOSITE AIRCRAFT STRUCTURES
Authors: RUBIN AM JERINA KL
Citation: Am. Rubin et Kl. Jerina, EVALUATION OF POROSITY IN COMPOSITE AIRCRAFT STRUCTURES, Mechanics of composite materials, 30(6), 1994, pp. 587-600
EVALUATION OF POROSITY IN COMPOSITE AIRCRAFT STRUCTURES
Authors: RUBIN AM JERINA KL
Citation: Am. Rubin et Kl. Jerina, EVALUATION OF POROSITY IN COMPOSITE AIRCRAFT STRUCTURES, Composites engineering, 3(7-8), 1993, pp. 601
DEFORMATION CHARACTERISTICS OF THE RAPIDLY SOLIDIFIED AL-8.5-PERCENT FE-1.2-PERCENT V-1.7-PERCENT SI ALLOY
Authors: HARIPRASAD S SASTRY SML JERINA KL
Citation: S. Hariprasad et al., DEFORMATION CHARACTERISTICS OF THE RAPIDLY SOLIDIFIED AL-8.5-PERCENT FE-1.2-PERCENT V-1.7-PERCENT SI ALLOY, Scripta metallurgica et materialia, 29(4), 1993, pp. 463-466
PREPARATION BY DIFFUSION BONDING AND ADHESIVE BONDING OF ALUMINUM-ALLOY SPECIMENS FOR FRACTURE-TOUGHNESS AND FATIGUE-CRACK GROWTH RESISTANCE MEASUREMENTS IN DIFFERENT ORIENTATIONS
Authors: HARIPRASAD S SASTRY SML JERINA KL
Citation: S. Hariprasad et al., PREPARATION BY DIFFUSION BONDING AND ADHESIVE BONDING OF ALUMINUM-ALLOY SPECIMENS FOR FRACTURE-TOUGHNESS AND FATIGUE-CRACK GROWTH RESISTANCE MEASUREMENTS IN DIFFERENT ORIENTATIONS, Materials science & engineering. A, Structural materials: properties, microstructure and processing, 169(1-2), 1993, pp. 120000013-120000016
Risultati: 1-18 |