Optimization of Hypersonic Airbreathing Propulsion Systems through Mixed Analysis Methods
Accurate flow path modeling of scramjet engines is a key step in the development of an airframe integrated engine for hypersonic vehicles. A scramjet system model architecture is proposed and implemented using three different engine components: the isolator, combustor, and nozzle. For each component...
Main Author: | DellaFera, Andrew Brian |
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Other Authors: | Aerospace and Ocean Engineering |
Format: | Others |
Published: |
Virginia Tech
2019
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Subjects: | |
Online Access: | http://hdl.handle.net/10919/95512 |
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