R Hackney, T Nikolaidis, A Pellegrini - Applied Thermal Engineering, 2020 - Elsevier
The modelling of compressor interstage bleed in a gas turbine is required at all phases of the engine design cycle. The effect of the physical geometry of the bleed offtake on …
S Reitenbach, M Schnoes… - … Expo: Power for …, 2015 - asmedigitalcollection.asme.org
Variable geometry blade rows are a common instrument to avoid compressor instabilities which occur especially at low-and full-speed operation of gas turbines. The operating …
Gas turbine is a complex product of multidisciplinary coupling, which is known as the Pearl in the crown of equipment manufacturing industry. Forward design is the key technology of …
C Islam, Y Altintas - Journal of Manufacturing …, 2019 - asmedigitalcollection.asme.org
Prediction of temperature in the tool, chip, and workpiece surface is important to study tool wear, residual stresses in the machined part, and to design cutting tool substrates and …
O Ogunbodede, S Nandi… - Journal of …, 2019 - asmedigitalcollection.asme.org
Unmanned aerial vehicles (UAVs) are making increasingly long flights today with significantly longer mission times. This requires the UAVs to have long endurance as well as …
S Reitenbach, M Siggel, M Bolemant - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
This paper presents a novel approach to the development of an intelligent workflow engine utilising an artificial intelligence (AI) chatbot. The proposed system combines the …
I Kolias, A Alexiou, N Aretakis… - International Journal of …, 2021 - mdpi.com
A mean-line compressor performance calculation method is presented that covers the entire operating range, including the choked region of the map. It can be directly integrated into …
This paper presents a fully automated methodology to create start values for gas turbine performance computer programs. The methodology employs the application of evolutionary …