CHARACTERIZATION OF AN INTEGRATED NOZZLE, SUPERSONIC AXIAL TURBINE WITH A ROTATING DETONATION COMBUSTOR

von Braun, James
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Pressure gain combustion (2019)

GT2021-59702 Uncertainty in High-Pressure Stator Performance Measurement in an Annular Cascade at Engine-Representative Reynolds and Mach

von Bhatnagar, Lakshya
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 4: Controls, diagnostics, and instrumentation; cycle innovations; cycle innovations: energy storage; education; electric power (2021)

TURBINE-INTEGRATED HIGH-PRESSURE OPTICAL RDE (THOR) FOR INJECTION, DETONATION DYNAMICS ASSESSMENT

von Athmanathan, Venkat
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Pressure gain combustion (2019)

GT2020-15013 Particle Image Velocimetry in a High-Pressure Turbine Stage at Aerodynamically Engine Representative Conditions

von Inman, Daniel
Veröffentlicht in ASME Turbo Expo (2020 : Online) Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition - 2020 ; Volume 5: Controls, diagnostics, and instrumentation - cycle innovation - cycle innovations: energy storage (2020)

GT2021-59886 Development of a Lifetime Pressure Sensitive Paint Procedure for High-Pressure Vane Testing

von Aye-Addo, Papa Aye N.
Veröffentlicht in ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 4: Controls, diagnostics, and instrumentation; cycle innovations; cycle innovations: energy storage; education; electric power (2021)

PURDUE SMALL TURBINE AEROTHERMAL ROTATING RIG (STARR)

von Cuadrado, David G.
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Gas turbine engines ; Volume 1 of 2 (2019)