Methodology Development and Investigation of Turbofan Engine Response to Simultaneous Inlet Total Pressure and Swirl Distortion
As a contribution to advancing turbofan engine ground test technology in support of propulsion system integration in modern conceptual aircraft, a novel inlet distortion generator (ScreenVaneTM) was invented. The device simultaneously reproduces combined inlet total pressure and swirl distortion el...
Main Author: | Frohnapfel, Dustin Joseph |
---|---|
Other Authors: | Mechanical Engineering |
Format: | Others |
Published: |
Virginia Tech
2019
|
Subjects: | |
Online Access: | http://hdl.handle.net/10919/88866 |
Similar Items
-
Experimental Investigation of Fan Rotor Response to Inlet Swirl Distortion
by: Frohnapfel, Dustin Joseph
Published: (2016) -
A New Method for Generating Swirl Inlet Distortion for Jet Engine Research
by: Hoopes, Kevin M.
Published: (2014) -
Fluid Dynamics of Inlet Swirl Distortions for Turbofan Engine Research
by: Guimaraes Bucalo, Tamara
Published: (2018) -
Effect of BLI-Type Inlet Distortion on Turbofan Engine Performance
by: Lucas, James Redmond
Published: (2013) -
High Fidelity Time Accurate CFD Analysis of a Multi-stage Turbofan at Various Operating Points in Distorted Inflow
by: Weston, David Bruce
Published: (2014)