June 7th, 2021, 12:15 PM EDT - 1:45 PM EDT
Aircraft Engine Track
Deep Dive:
12:15 - 12:45 PM EDT, Paper No. GT2021-59079, “Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation”
Deep Dive:
12:45 - 1:15 PM EDT, Paper No. GT2021-58829, “Fan-Intake Coupling With Conventional and Short Intakes”
Rapid Talk:
1:15 - 1:25 PM EDT, Paper No. GT2021-60335, “A Study on the Aerodynamic Characteristics of a Blended-Wing-Body Aircraft With a Serpentine Inlet Using Flow Control Techniques”
Rapid Talk:
1:25 - 1:35 PM EDT, Paper No. GT2021-60230, “Investigation of a Passive Flow Control Device in an S-Duct Inlet at High Subsonic Flow”
Rapid Talk:
1:35 - 1:45 PM EDT, Paper No. GT2021-58849, “Internal Aerodynamic Performance Evaluation of a Double Entrance S-Duct Intake at High Subsonic Conditions”
This session contains papers that examine aircraft engine concepts of recent interest – boundary layer ingestion and short intake nacelles – that may eventually play a key part on their own or as part of novel hybrid systems to provide significant reductions in fuel burn and emissions. It also contains three papers that provide recent insights on the aerodynamic characteristics of serpentine or S-duct inlets to include passive and active flow control techniques.
Presentations
Participant Role | Details | Action |
---|---|---|
Submission | Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation | View |
Submission | Fan-Intake Coupling With Conventional and Short Intakes | View |
Submission | A Study on the Aerodynamic Characteristics of a Blended-Wing-Body Aircraft With a Serpentine Inlet Using Flow Control Techniques | View |
Submission | Investigation of a Passive Flow Control Device in an S-Duct Inlet at High Subsonic Flow | View |
Submission | Internal Aerodynamic Performance Evaluation of a Double Entrance S-Duct Intake at High Subsonic Conditions | View |