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 language | English |
|---|---|
| Pages (from-to) | 697-704 |
| Number of pages | 8 |
| Journal | Journal of Propulsion and Power |
| Volume | 16 |
| Issue number | 4 |
| DOIs | |
| Publication status | Published - 2000 Jan 1 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Fuel Technology
- Mechanical Engineering
- Space and Planetary Science
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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 journal › Article
TY - JOUR
T1 - Numerical investigation of installation effects in turbofan engines
AU - Joo, W. G.
PY - 2000/1/1
Y1 - 2000/1/1
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=0034227706&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0034227706&partnerID=8YFLogxK
U2 - 10.2514/2.5629
DO - 10.2514/2.5629
M3 - Article
AN - SCOPUS:0034227706
VL - 16
SP - 697
EP - 704
JO - Journal of Propulsion and Power
JF - Journal of Propulsion and Power
SN - 0748-4658
IS - 4
ER -