Startseite Technik Power Conversion System Considerations for an Advanced Nuclear Gas Turbine (GT-VHTR) CHHP Demonstration Plant Concept
Artikel
Lizenziert
Nicht lizenziert Erfordert eine Authentifizierung

Power Conversion System Considerations for an Advanced Nuclear Gas Turbine (GT-VHTR) CHHP Demonstration Plant Concept

  • Colin G. McDonald,
Veröffentlicht/Copyright: 1. Dezember 2010
Veröffentlichen auch Sie bei De Gruyter Brill
Informationen für Autor*innen
International Journal of Turbo and Jet Engines
Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 27 Heft 3-4

Published Online: 2010-12

©2011 by Walter de Gruyter GmbH & Co.

Artikel in diesem Heft

  1. CONTENTS
  2. Computer Simulation of Performance and Economic Assessment of a Single Shaft Gas Turbine Combined Heat Cooling and Power Plant
  3. Performance Assessment of Single and Two Shaft Gas Industrial Turbines Using Fuels of Different Calorific Values
  4. Power Conversion System Considerations for an Advanced Nuclear Gas Turbine (GT-VHTR) CHHP Demonstration Plant Concept
  5. Development of a Multiobjective Optimization Method for Aerospace Turbopump Design
  6. A Mixed Data-Driven and Model Based Fault Classification for Gas Turbine Diagnosis
  7. Startup Simulation of Twin Spool Turbofan Engine
  8. A Computational Investigation of Icing Effects on an S-Duct Inlet
https://doi.org/10.1515/TJJ.2010.27.3-4.179

Artikel in diesem Heft

  1. CONTENTS
  2. Computer Simulation of Performance and Economic Assessment of a Single Shaft Gas Turbine Combined Heat Cooling and Power Plant
  3. Performance Assessment of Single and Two Shaft Gas Industrial Turbines Using Fuels of Different Calorific Values
  4. Power Conversion System Considerations for an Advanced Nuclear Gas Turbine (GT-VHTR) CHHP Demonstration Plant Concept
  5. Development of a Multiobjective Optimization Method for Aerospace Turbopump Design
  6. A Mixed Data-Driven and Model Based Fault Classification for Gas Turbine Diagnosis
  7. Startup Simulation of Twin Spool Turbofan Engine
  8. A Computational Investigation of Icing Effects on an S-Duct Inlet
Jetzt anmelden und 20% sparen
Institutioneller Zugang
Wie funktioniert Authentifizierung?
Haben Sie eine Idee, wie wir unsere Website verbessern können?
Bitte schreiben Sie uns.
© 2026 De Gruyter Brill
Heruntergeladen am 19.1.2026 von https://www.degruyterbrill.com/document/doi/10.1515/TJJ.2010.27.3-4.179/pdf
Button zum nach oben scrollen