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Proc. ASME. GT2021, Volume 1: Aircraft Engine; Fans and Blowers; Marine; Wind Energy; Scholar Lecture, V001T01A017, June 7–11, 2021
Paper No: GT2021-60029
..., England, University of Babylon, Cranfield, Bedford, UK UK Faculty of Engineering- Bedfordshire, England, Musayib UK Babil, Iraq ABSTRACT The use of a simulation tool to predict the aero-engine NOMENCLATURE performance before committing to a final engine design has Abp Bypass nozzle area, [m2] become one...
Proc. ASME. GT2021, Volume 1: Aircraft Engine; Fans and Blowers; Marine; Wind Energy; Scholar Lecture, V001T41A001, June 7–11, 2021
Paper No: GT2021-60864
... Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-60864 INSTABILITIES EVERYWHERE! HARD PROBLEMS IN AERO-ENGINES Zoltán S. Spakovszky Massachusetts Institute of Technology Cambridge, MA 02138 ABSTRACT NOMENCLATURE...
Proc. ASME. GT2020, Volume 5: Controls, Diagnostics, and Instrumentation; Cycle Innovations; Cycle Innovations: Energy Storage, V005T05A004, September 21–25, 2020
Paper No: GT2020-14278
...Abstract Abstract The reliability and safety of aero-engine are often the decisive factors for the safe and reliable flight of commercial aircraft. Hence, the vibration source location and fault diagnosis of aero-engine are of prime importance to detect faults and carry out fast and effective...
Proc. ASME. GT2020, Volume 10B: Structures and Dynamics, V10BT27A027, September 21–25, 2020
Paper No: GT2020-16259
... reflects the physical essence of the rotor burst more realistically and can be simply verified without requiring too much test data, therefore it has a good application prospect in the aircraft engine airworthiness. aero-engine airworthiness overspeed burst strain-based fracture criteria...
Proc. ASME. GT2020, Volume 1: Aircraft Engine; Fans and Blowers, V001T01A024, September 21–25, 2020
Paper No: GT2020-15119
... actuator of the nozzle formed by numerical simulation has faster response, and good dynamic characteristics. It has certain guiding significance for follow-up research. Keywords: Integrated simulation; propelling nozzle; fuzzy PI control; aero-engine; NOMENCLATURE 8A Throat area of the propelling nozzle...