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Results: 1-15 |
Results: 15
COUPLING OF TWIN RECTANGULAR SUPERSONIC JETS
Authors: RAMAN G TAGHAVI R
Citation: G. Raman et R. Taghavi, COUPLING OF TWIN RECTANGULAR SUPERSONIC JETS, Journal of Fluid Mechanics, 354, 1998, pp. 123-146
INFORMATION-PROCESSING IN RECOVERED DEPRESSED CHILDREN AND ADOLESCENTS
Authors: DALGLEISH T NESHATDOOST H TAGHAVI R MORADI A YULE W CANTERBURY R VOSTANIS P
Citation: T. Dalgleish et al., INFORMATION-PROCESSING IN RECOVERED DEPRESSED CHILDREN AND ADOLESCENTS, Journal of child psychology and psychiatry and allied disciplines, 39(7), 1998, pp. 1031-1035
AEROACOUSTIC CHARACTERISTICS OF A RECTANGULAR MULTIELEMENT SUPERSONICJET MIXER-EJECTOR NOZZLE
Authors: RAMAN G TAGHAVI R
Citation: G. Raman et R. Taghavi, AEROACOUSTIC CHARACTERISTICS OF A RECTANGULAR MULTIELEMENT SUPERSONICJET MIXER-EJECTOR NOZZLE, Journal of sound and vibration, 207(2), 1997, pp. 227
INFORMATION-PROCESSING IN CLINICALLY DEPRESSED AND ANXIOUS CHILDREN AND ADOLESCENTS
Authors: DALGLEISH T TAGHAVI R NESHATDOOST H MORADI A YULE W CANTERBURY R
Citation: T. Dalgleish et al., INFORMATION-PROCESSING IN CLINICALLY DEPRESSED AND ANXIOUS CHILDREN AND ADOLESCENTS, Journal of child psychology and psychiatry and allied disciplines, 38(5), 1997, pp. 535-541
FLOW CHARACTERISTICS OF A RECTANGULAR MULTIELEMENT SUPERSONIC MIXER-EJECTOR
Authors: TAGHAVI R RAMAN G
Citation: R. Taghavi et G. Raman, FLOW CHARACTERISTICS OF A RECTANGULAR MULTIELEMENT SUPERSONIC MIXER-EJECTOR, Journal of propulsion and power, 12(5), 1996, pp. 1004-1007
VISUALIZATION OF SUPERSONIC SCREECHING JETS USING A PHASE CONDITIONEDFOCUSING SCHLIEREN SYSTEM
Authors: TAGHAVI R RAMAN G
Citation: R. Taghavi et G. Raman, VISUALIZATION OF SUPERSONIC SCREECHING JETS USING A PHASE CONDITIONEDFOCUSING SCHLIEREN SYSTEM, Experiments in fluids, 20(6), 1996, pp. 472-475
AUTOMATIC, PARALLEL AND FAULT-TOLERANT MESH GENERATION FROM CAD
Authors: TAGHAVI R
Citation: R. Taghavi, AUTOMATIC, PARALLEL AND FAULT-TOLERANT MESH GENERATION FROM CAD, Engineering with computers, 12(3-4), 1996, pp. 178-185
RESONANT INTERACTION OF A LINEAR-ARRAY OF SUPERSONIC RECTANGULAR JETS- AN EXPERIMENTAL-STUDY (VOL 309, PG 93, 1996)
Authors: RAMAN G TAGHAVI R
Citation: G. Raman et R. Taghavi, RESONANT INTERACTION OF A LINEAR-ARRAY OF SUPERSONIC RECTANGULAR JETS- AN EXPERIMENTAL-STUDY (VOL 309, PG 93, 1996), Journal of Fluid Mechanics, 326, 1996, pp. 437-437
RESONANT INTERACTION OF A LINEAR-ARRAY OF SUPERSONIC RECTANGULAR JETS- AN EXPERIMENTAL-STUDY
Authors: RAMAN G TAGHAVI R
Citation: G. Raman et R. Taghavi, RESONANT INTERACTION OF A LINEAR-ARRAY OF SUPERSONIC RECTANGULAR JETS- AN EXPERIMENTAL-STUDY, Journal of Fluid Mechanics, 309, 1996, pp. 93-111
APPLICATION OF PRESSURE-SENSITIVE PAINT IN SUPERSONIC NOZZLE RESEARCH
Authors: CLER D LAMB M FAROKHI S TAGHAVI R HAZLEWOOD R
Citation: D. Cler et al., APPLICATION OF PRESSURE-SENSITIVE PAINT IN SUPERSONIC NOZZLE RESEARCH, Journal of aircraft, 33(6), 1996, pp. 1109-1114
DOES KIDNEY DONATION THREATEN THE QUALITY-OF-LIFE OF THE DONOR
Authors: TAGHAVI R
Citation: R. Taghavi, DOES KIDNEY DONATION THREATEN THE QUALITY-OF-LIFE OF THE DONOR, Transplantation proceedings, 27(5), 1995, pp. 2595-2596
THE EFFECT OF PREOPERATIVE STRUCTURED TEACHING ON RENAL-TRANSPLANTATION OUTCOME
Authors: TAGHAVI R
Citation: R. Taghavi, THE EFFECT OF PREOPERATIVE STRUCTURED TEACHING ON RENAL-TRANSPLANTATION OUTCOME, Transplantation proceedings, 27(5), 1995, pp. 2597-2598
FREQUENCY-DOMAIN ANALYSIS OF FLUCTUATING PRESSURE ON A PUSHER PROPELLER BLADE SURFACE
Authors: FAROKHI S TAGHAVI R WETZEL KK
Citation: S. Farokhi et al., FREQUENCY-DOMAIN ANALYSIS OF FLUCTUATING PRESSURE ON A PUSHER PROPELLER BLADE SURFACE, Journal of aircraft, 31(1), 1994, pp. 42-48
ENHANCED MIXING OF MULTIPLE SUPERSONIC RECTANGULAR JETS BY SYNCHRONIZED SCREECH
Authors: TAGHAVI R RAMAN G
Citation: R. Taghavi et G. Raman, ENHANCED MIXING OF MULTIPLE SUPERSONIC RECTANGULAR JETS BY SYNCHRONIZED SCREECH, AIAA journal, 32(12), 1994, pp. 2477-2480
COMPUTATIONAL STUDY OF ADVANCED EXHAUST SYSTEM TRANSITION DUCTS WITH EXPERIMENTAL VALIDATION
Authors: WU C FAROKHI S TAGHAVI R
Citation: C. Wu et al., COMPUTATIONAL STUDY OF ADVANCED EXHAUST SYSTEM TRANSITION DUCTS WITH EXPERIMENTAL VALIDATION, Journal of propulsion and power, 9(3), 1993, pp. 437-442
Risultati: 1-15 |