Numerical investigation of installation effects in turbofan engines

Research output: Contribution to journalArticle

1 Citation (Scopus)

Abstract

One of the important issues in the assessment of intake/engine compatibility in civil turbofan engines is the prediction of the coupling effects between the intake and the engine. An actuator-disk model has been applied to the calculations of the flow through a high-bypass-ratio turbofan geometry, including the presence of the core-support pylon and a nonaxisymmetric inlet, and the effects of the core engine. The results of a series of calculations are presented, and the nature of the interactions between the flow through a fan and the system components is addressed.

Original languageEnglish
Pages (from-to)697-704
Number of pages8
JournalJournal of Propulsion and Power
Volume16
Issue number4
DOIs
Publication statusPublished - 2000 Jan 1

Fingerprint

turbofan engines
Turbofan engines
installing
engines
engine
Engines
actuator disks
bypass ratio
pylons
turbofans
Actuator disks
Bypass ratio
fans
compatibility
Fans
bypass
Geometry
geometry
predictions
effect

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Fuel Technology
  • Mechanical Engineering
  • Space and Planetary Science

Cite this

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Numerical investigation of installation effects in turbofan engines. / Joo, W. G.

In: Journal of Propulsion and Power, Vol. 16, No. 4, 01.01.2000, p. 697-704.

Research output: Contribution to journalArticle

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