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Small Turbojet Exhaust Nozzle with Optimal Geometry and Integrated Exit Guide Vanes

BACKGROUND Small scale turbojets are used for various applications amongst the military and commercial industry. Given their diverse capability, these engines need to perform at an optimal level to maintain success in their missions. The purpose of the presented design is to improve the thrust-to-weight ratio of a small turbojet engine by only...

Published: 5/10/2024 | Inventor(s): Colton Swart, Thomas Coulon, Grant Schumacher, Lauren Jones, Kurt Rouser

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Category(s): Technology Classifications > Engineering > Mechanical & Aerospace Engr, Technology Classifications > Unmanned Systems