Forced response predictions for a HP turbine rotor blade
- Author
- VAHDATI, M1 ; GREEN, J2 ; MARSHALL, J. G2 ; IMREGUN, M1
[1] Imperial College, MED, Exhibition Road, London SW7 2BX, United Kingdom
[2] Rolls-Royce plc, P.O. Box 31, Moor Lane (ML-83), Derby DE24 8BJ, United Kingdom - Conference title
- Design principles and methods for aircraft gas turbine engines (Toulouse, 11-15 May 1998) = Les principes et méthodes de conception des turbomoteurs (fr)
- Conference name
- RTO applied vehicle technology panel symposium (Toulouse 1998-05-11)
- Source
RTO Meeting proceedings. 1999, pp 34.1-34.11 ; ref : 18 ref
- ISBN
- 92-837-0005-8
- Scientific domain
- Energy; Mechanical engineering
- Publisher
- Research and Technology Organization, Neuilly-sur-Seine
- Publication country
- France
- Document type
- Conference Paper
- Language
- English
- Keyword (fr)
- Aéroélasticité Ecoulement instationnaire Etage turbine Haute pression Modélisation Turbine gaz Vibration forcée
- Keyword (en)
- Aeroelasticity Unsteady flow Turbine stage High pressure Modeling Gas turbine Forced vibration
- Keyword (es)
- Aeroelasticidad Flujo inuniforme Etapa turbina Alta presión Modelización Turbina gas Vibración forzada
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40F Solid mechanics / 001B40F30 Structural and continuum mechanics / 001B40F30M Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D12 Mechanical engineering. Machine design / 001D12F Engines and turbines / 001D12F02 Continuous cycle engines: steam and gas turbines, jet engines
- Discipline
- Mechanical engineering. Mechanical construction. Handling Physics : solid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 1810221
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
Install on your browser
"O:13:\"PanistOpenUrl\":36:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000idc\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:0:\"\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:9:\"\u0000*\u0000jtitle\";s:23:\"RTO Meeting proceedings\";s:9:\"\u0000*\u0000stitle\";s:0:\"\";s:7:\"\u0000*\u0000date\";s:4:\"1999\";s:9:\"\u0000*\u0000volume\";s:0:\"\";s:8:\"\u0000*\u0000issue\";s:0:\"\";s:8:\"\u0000*\u0000spage\";s:4:\"34.1\";s:8:\"\u0000*\u0000epage\";s:5:\"34.11\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:0:\"\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"VAHDATI\";s:10:\"\u0000*\u0000aufirst\";s:1:\"M\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:8:\"GREEN, J\";i:1;s:14:\"MARSHALL, J. G\";i:2;s:10:\"IMREGUN, M\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:13:\"92-837-0005-8\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:89:\"Design principles and methods for aircraft gas turbine engines (Toulouse, 11-15 May 1998)\";s:8:\"\u0000*\u0000title\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:8:\"\u0000*\u0000place\";s:17:\"Neuilly-sur-Seine\";s:6:\"\u0000*\u0000pub\";s:36:\"Research and Technology Organization\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:0:\"\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Panist access
"O:12:\"IstexOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:0:\"\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:9:\"\u0000*\u0000jtitle\";s:23:\"RTO Meeting proceedings\";s:9:\"\u0000*\u0000stitle\";s:0:\"\";s:7:\"\u0000*\u0000date\";s:4:\"1999\";s:9:\"\u0000*\u0000volume\";s:0:\"\";s:8:\"\u0000*\u0000issue\";s:0:\"\";s:8:\"\u0000*\u0000spage\";s:4:\"34.1\";s:8:\"\u0000*\u0000epage\";s:5:\"34.11\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:0:\"\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"VAHDATI\";s:10:\"\u0000*\u0000aufirst\";s:1:\"M\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:8:\"GREEN, J\";i:1;s:14:\"MARSHALL, J. G\";i:2;s:10:\"IMREGUN, M\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:13:\"92-837-0005-8\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:89:\"Design principles and methods for aircraft gas turbine engines (Toulouse, 11-15 May 1998)\";s:8:\"\u0000*\u0000title\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:8:\"\u0000*\u0000place\";s:17:\"Neuilly-sur-Seine\";s:6:\"\u0000*\u0000pub\";s:36:\"Research and Technology Organization\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:0:\"\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Istex access
"O:16:\"EuropePMCOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:0:\"\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:9:\"\u0000*\u0000jtitle\";s:23:\"RTO Meeting proceedings\";s:9:\"\u0000*\u0000stitle\";s:0:\"\";s:7:\"\u0000*\u0000date\";s:4:\"1999\";s:9:\"\u0000*\u0000volume\";s:0:\"\";s:8:\"\u0000*\u0000issue\";s:0:\"\";s:8:\"\u0000*\u0000spage\";s:4:\"34.1\";s:8:\"\u0000*\u0000epage\";s:5:\"34.11\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:0:\"\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"VAHDATI\";s:10:\"\u0000*\u0000aufirst\";s:1:\"M\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:8:\"GREEN, J\";i:1;s:14:\"MARSHALL, J. G\";i:2;s:10:\"IMREGUN, M\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:13:\"92-837-0005-8\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:89:\"Design principles and methods for aircraft gas turbine engines (Toulouse, 11-15 May 1998)\";s:8:\"\u0000*\u0000title\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:8:\"\u0000*\u0000place\";s:17:\"Neuilly-sur-Seine\";s:6:\"\u0000*\u0000pub\";s:36:\"Research and Technology Organization\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:0:\"\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Europe PubMed Central access
"O:11:\"BaseOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:0:\"\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:9:\"\u0000*\u0000jtitle\";s:23:\"RTO Meeting proceedings\";s:9:\"\u0000*\u0000stitle\";s:0:\"\";s:7:\"\u0000*\u0000date\";s:4:\"1999\";s:9:\"\u0000*\u0000volume\";s:0:\"\";s:8:\"\u0000*\u0000issue\";s:0:\"\";s:8:\"\u0000*\u0000spage\";s:4:\"34.1\";s:8:\"\u0000*\u0000epage\";s:5:\"34.11\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:0:\"\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"VAHDATI\";s:10:\"\u0000*\u0000aufirst\";s:1:\"M\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:8:\"GREEN, J\";i:1;s:14:\"MARSHALL, J. G\";i:2;s:10:\"IMREGUN, M\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:13:\"92-837-0005-8\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:89:\"Design principles and methods for aircraft gas turbine engines (Toulouse, 11-15 May 1998)\";s:8:\"\u0000*\u0000title\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:8:\"\u0000*\u0000place\";s:17:\"Neuilly-sur-Seine\";s:6:\"\u0000*\u0000pub\";s:36:\"Research and Technology Organization\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:0:\"\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
Base Search access
"O:12:\"ArXivOpenUrl\":35:{s:10:\"\u0000*\u0000openUrl\";N;s:6:\"\u0000*\u0000fmt\";s:10:\"proceeding\";s:6:\"\u0000*\u0000doi\";s:0:\"\";s:6:\"\u0000*\u0000pii\";s:0:\"\";s:7:\"\u0000*\u0000pmid\";s:0:\"\";s:9:\"\u0000*\u0000atitle\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:9:\"\u0000*\u0000jtitle\";s:23:\"RTO Meeting proceedings\";s:9:\"\u0000*\u0000stitle\";s:0:\"\";s:7:\"\u0000*\u0000date\";s:4:\"1999\";s:9:\"\u0000*\u0000volume\";s:0:\"\";s:8:\"\u0000*\u0000issue\";s:0:\"\";s:8:\"\u0000*\u0000spage\";s:4:\"34.1\";s:8:\"\u0000*\u0000epage\";s:5:\"34.11\";s:8:\"\u0000*\u0000pages\";s:0:\"\";s:7:\"\u0000*\u0000issn\";s:0:\"\";s:8:\"\u0000*\u0000eissn\";s:0:\"\";s:9:\"\u0000*\u0000aulast\";s:7:\"VAHDATI\";s:10:\"\u0000*\u0000aufirst\";s:1:\"M\";s:9:\"\u0000*\u0000auinit\";s:0:\"\";s:10:\"\u0000*\u0000auinitm\";s:0:\"\";s:5:\"\u0000*\u0000au\";a:3:{i:0;s:8:\"GREEN, J\";i:1;s:14:\"MARSHALL, J. G\";i:2;s:10:\"IMREGUN, M\";}s:9:\"\u0000*\u0000aucorp\";s:0:\"\";s:7:\"\u0000*\u0000isbn\";s:13:\"92-837-0005-8\";s:8:\"\u0000*\u0000coden\";s:0:\"\";s:8:\"\u0000*\u0000genre\";s:10:\"proceeding\";s:7:\"\u0000*\u0000part\";s:0:\"\";s:9:\"\u0000*\u0000btitle\";s:89:\"Design principles and methods for aircraft gas turbine engines (Toulouse, 11-15 May 1998)\";s:8:\"\u0000*\u0000title\";s:56:\"Forced response predictions for a HP turbine rotor blade\";s:8:\"\u0000*\u0000place\";s:17:\"Neuilly-sur-Seine\";s:6:\"\u0000*\u0000pub\";s:36:\"Research and Technology Organization\";s:10:\"\u0000*\u0000edition\";s:0:\"\";s:9:\"\u0000*\u0000tpages\";s:0:\"\";s:9:\"\u0000*\u0000series\";s:0:\"\";s:8:\"\u0000*\u0000proxy\";s:30:\"http:\/\/proxyout.inist.fr:8080\/\";s:12:\"\u0000*\u0000integrite\";b:1;}"
arXiv access
