Publication Date:
2019-07-13
Description:
The objective of this study was to demonstrate the capability to analyze the aerodynamic performance of the complete low pressure subsystem (LPS) of the Energy Efficient Engine (EEE). Detailed analyses were performed using three- dimensional Navier-Stokes numerical models employing advanced clustered processor computing platforms. The analysis evaluates the impact of steady aerodynamic interaction effects between the components of the LPS at design and off- design operating conditions. Mechanical coupling is provided by adjusting the rotational speed of common shaft-mounted components until a power balance is achieved. The Navier-Stokes modeling of the complete low pressure subsystem provides critical knowledge of component acro/mechanical interactions that previously were unknown to the designer until after hardware testing.
Keywords:
Aircraft Propulsion and Power
Type:
NASA/TM-1998-208402
,
E-11234
,
NAS 1.15:208402
,
AIAA Paper 98-3119
,
Propulsion; Jul 13, 1998 - Jul 15, 1998; Cleveland, OH; United States
Format:
application/pdf
