Startseite Technik Spray Characteristics of Two Combined Jet Atomizers
Artikel
Lizenziert
Nicht lizenziert Erfordert eine Authentifizierung

Spray Characteristics of Two Combined Jet Atomizers

  • Y. Tambour, und D. Portnoy,
Veröffentlicht/Copyright: 1. Dezember 1985
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 2 Heft 4

Published Online: 1985-12

©2011 by Walter de Gruyter GmbH & Co.

Artikel in diesem Heft

  1. CONTENTS
  2. Prediciton of Flow in Rotating Disc Systems Using the k-є Turbulence Model
  3. Spray Characteristics of Two Combined Jet Atomizers
  4. Nozzle Design and Integration in an Advanced Supersonic Fighter
  5. Mass Flow Limitation of Supersonic Blade Rows Due to Leading Edge Blockage
  6. Effect of Free Stream Turbulence on Flow Separation
  7. Effect of Aspect Ratio on Energy Loss in Nozzle Blades of Small Power Turbines
  8. A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery
  9. The Role of the Heat-up Period in Fuel Drop Evaporation
  10. Advanced Concepts in Small Helicopter Engine Air-Cooled Turbine Design
  11. The Influence of Different Geometries for a Vaned Diffuser on the Pressure Distribution in a Centrifugal Compressor
  12. Computer Calculation of Fan Erosion in Coal-fired Power Plants. Part 2: Axial Fans
https://doi.org/10.1515/TJJ.1985.2.4.263

Artikel in diesem Heft

  1. CONTENTS
  2. Prediciton of Flow in Rotating Disc Systems Using the k-є Turbulence Model
  3. Spray Characteristics of Two Combined Jet Atomizers
  4. Nozzle Design and Integration in an Advanced Supersonic Fighter
  5. Mass Flow Limitation of Supersonic Blade Rows Due to Leading Edge Blockage
  6. Effect of Free Stream Turbulence on Flow Separation
  7. Effect of Aspect Ratio on Energy Loss in Nozzle Blades of Small Power Turbines
  8. A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery
  9. The Role of the Heat-up Period in Fuel Drop Evaporation
  10. Advanced Concepts in Small Helicopter Engine Air-Cooled Turbine Design
  11. The Influence of Different Geometries for a Vaned Diffuser on the Pressure Distribution in a Centrifugal Compressor
  12. Computer Calculation of Fan Erosion in Coal-fired Power Plants. Part 2: Axial Fans
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 25.2.2026 von https://www.degruyterbrill.com/document/doi/10.1515/TJJ.1985.2.4.263/html
Button zum nach oben scrollen