Variable Area Nozzle T50-BO-8A Turbojet

The goal of this project was to design, build and test a variable area nozzle using a Boeing T50-BO-8A turbojet engine. Engineering performed piece-part design, thermal analysis and generated a 3D CAD model. The nozzle was fabricated from Inconel 718 and utilized a hydraulic control system to vary nozzle exit area. The engine/nozzle was tested; data was analyzed and is now currently being used in laboratory experiments at California Polytechnic State University, San Luis Obispo.

Research & Development Capabilities:

· Laboratory Instrumentation
· Failure Mode testing
· Process Engineering
· Experimental Fixture Design
· Sensor Applications
· Feasibility Studies
· Load Data Acquisition
· Experimental Structure Design
· Material Coupon Testing