Design of new three stage low pressure turbine for the bmw rolls-royce BR715 turbofan engine

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1997, Pages

  Cobley, Keith ^a   Coleman, Neil ^a   Siden, Gunnar ^b   Arndt, Norbert ^b  

^a ROLLS ROYCE PLC   (United Kingdom)

^b Rolls Royce Deutschland   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; AERODYNAMICS; AIRCRAFT ENGINES; ENGINES; GAS TURBINES; MARINE ENGINES;

ADVANCED TECHNOLOGY; DELIVERY TIMESCALES; DEVELOPMENT PROGRAMMES; ENGINE DEVELOPMENT; LOW PRESSURE SYSTEMS; LOW-PRESSURE TURBINES; MODULE CONFIGURATIONS; SIMULTANEOUS DESIGNS;

DESIGN;

EID: 84973645502     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-419     Document Type: Conference Paper

References (12)

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9. Schulte V and Hodson HP, 1996 "Unsteady Wake-Induced Boundary Layer Transisition in High Lift LP Turbines" ASME 96-GT-486.
10. Halstead DE, Wisler DC, Okiishi TH, Walker GJ, Hodson HP, Shin HW, 1995 "Boundary Layer Development in Axial Compressors and Turbines part 1 of 4; Composite Picture" ASME 95-GT-461.
11. Schulte V and Hodson HP, "Prediction of the Becalmed Region for LP Turbine Profile Design" to be presented at the ASME Turbo EXPO 97 in Orlando, F.L.
12. Lapworth BL, 1993 "Three-Dimensional Mesh Embedding for the Navier-Stokes Equations using Upwind Control Volumes". Int. J. Numer. Meth. Fluids, 17, 195-220.