Installation Effects of Supersonic Inlets on Next-Generation SST Turbofan Engines

Installation Effects of Supersonic Inlets on Next-Generation SST Turbofan Engines

This study explores inlet-related installation effects on next-generation SST aircraft, focusing on supersonic business jets. Using a comprehensive framework with consistent thrust/drag bookkeeping and realistic modeling of inlet losses, including operational limits for “buzz” and distortions, the i...

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Bibliographic Details
Main Authors: Stylianos Adamidis, Dario Del Gatto, Christos Mourouzidis, Stephen Brown, Vassilios Pachidis
Format: Article
Language:English
Published: MDPI AG 2025-03-01
Series:Engineering Proceedings
Subjects:
supersonic inlet
installation losses
bypass airflow control system
spillage drag
bypass drag
total pressure recovery
Online Access:https://www.mdpi.com/2673-4591/90/1/50
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