Aeroelastic design of turbine blades - ADTurBII overview

ETC 2005 - 6th Conference on Turbomachinery: Fluid Dynamics and Thermodynamics

Volumn , Issue , 2005, Pages

  Elliott, R ^a   Green, J S ^a   Seinturier, E ^a  

^a ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ENGINES; FATIGUE OF MATERIALS; FLOW OF GASES; THERMODYNAMICS; TURBOMACHINERY; VIBRATION ANALYSIS;

AEROELASTIC DESIGNS; COLLABORATIVE PROJECTS; DESIGN AND ANALYSIS; EUROPEAN LEVELS; GEOMETRICAL VARIATIONS; HIGH CYCLE FATIGUE; MISTUNE EFFECTS; TURBINE BLADE;

TURBOMACHINE BLADES;

EID: 84925433403     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Plenary Session of 4th National Turbine Engine High Cycle Fatigue Conference, Monterey, USA. 1999. Mr Jim Newman, US Navy.
2. Plenary Session of 5th National Turbine Engine High Cycle Fatigue Conference, Phoenix, USA. 2000. Brig Gen Stan Sieg, US Air Force.
3. Robust Airfoils in Modern Gas Turbines (RAM-GT). EC 4th Framework Project: G4RD-CT-2000-00183. See www.cordis.lu
4. Green, J., 2000 ADTurB Synthesis Report, ADTurB-RR-0011. Available via www.cordis.lu or project website [6].
5. AB Stanbridge, IA Sever, DJ Ewins, Imperial College, London, U.K: Vibration measurements in a rotating blisk test rig using an LDV.
6. DLR website: www.dlr.de
7. ADTurB II project web site.: http://www.energy.kth.se/adturb2/
8. L DiMare, AI Sayma, J Green, M Imregun, Imperial College, London, U.K Low Engine Order Forced Response due to NGV Throat Width Variations
9. Genaro Scarselli, Leonardo Lecce, University of Naples, Italy Genetic Algorithms for the Evaluation of Mistune Effects on Turbomachinery
10. A Kessar, et al, KTH Stockholm, Sweden & DLR, Goettigen, Germany Flow Measurements for LEO Excitations in a High Pressure Turbine Stage
11. M Myhre, KTH Stockholm, Sweden Numerical investigation of Sensitivity of Forced Response Characteristics of Bladed Disk to Mistuning. Licenciate Thesis 2003.
12. A Berretta, F Rottmeier, P Ott, EPFL, Switzerland Combined/simultaneous gust and oscillating turbine row unsteady aerodynamics in subsonic Flow