Advanced Measurement Capability of Turbine Engine Exhaust and Jet Flows through Non-intrusive Methods

Advanced Air Force turbine engines with integrated engine exhaust systems require diagnostic flow measurements. Integration of these systems into altitude test cells creates problems with T&E requirements such as impingement problems, exhaust cooling spray blowback, acoustic emission issues and limited space for measurement systems. Propulsion system analysts need better understanding of low aspect ratio nozzles with serpentine flow paths.    Innovative non-intrusive flow measurements and data analysis techniques developed by UTSI fit this need but were traditionally fielded in wind tunnel or lab environments. This effort will utilize combined assets of Non-Contact Technologies (NCT) and University of Tennessee Space Institute (UTSI) to develop a commercial non-intrusive flow measurement capability to meet Air Force requirements. UTSI has developed non-intrusive, field-deployable flow measurement techniques and associated data reduction methodology, while NCT has experience in Dynamic Data Analysis, production of field ready, rugged equipment plus non-intrusive measurement experience. This solution will give major AEDC and Air Force stakeholders a capability that will fulfill the requirement for research in nozzle testing, provide a rugged system that is deployable in the field or an altitude test cell, and ensure AEDC and the Air Force can meet customer requirements due to the improved system diagnostic capability.