Design of a miniature hydrogen fueled gas turbine engine [PDF]
The design, development, and delivery of a miniature hydrogen-fueled gas turbine engine are discussed. The engine was to be sized to approximate a scaled-down lift engine such as the teledyne CAE model 376.
Burnett, M. +6 more
core +1 more source
Single-stage experimental evaluation of boundary layer blowing techniques for high lift stator blades. 1 - Compressor design [PDF]
Boundary layer blowing techniques for high lift stator blades in axial flow ...
Chapman, D. C., Miller, M. L.
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Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. Task 5: Unsteady counterrotation ducted propfan analysis [PDF]
The primary objective of this study was the development of a time-marching three-dimensional Euler/Navier-Stokes aerodynamic analysis to predict steady and unsteady compressible transonic flows about ducted and unducted propfan propulsion systems ...
Delaney, Robert A., Hall, Edward J.
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Explainable Reinforcement Learning for the Initial Design Optimization of Compressors Inspired by the Black-Winged Kite. [PDF]
Biomimetics (Basel)Zhang M, Miao Z, Nan X, Ma N, Liu R.
europepmc +1 more source
Small Engine Component Technology (SECT) [PDF]
A study of small gas turbine engines was conducted to identify high payoff technologies for year-2000 engines and to define companion technology plans.
Benn, K. +4 more
core +1 more source
A Multiscale Simulation and Experimental Study on the Microfog Evolution and Dust Control Mechanism Driven by Ultrasonic Atomization. [PDF]
ACS OmegaJiang Z +8 more
europepmc +1 more source
Challenges, Opportunities and Future Directions of Membrane Technology for Natural Gas Purification: A Critical Review. [PDF]
Membranes (Basel), 2022 Imtiaz A +6 more
europepmc +1 more source
Surging Limits of Multistage Axial-Flow Compressors.
TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, 1992 openaire +2 more sources
Modelling variable stator vane setting in multistage axial flow compressors
, 1998 A numerical approach for modelling variable stator stagger in multistage stage axial flow compressors is presented. The development of such an approach has been motivated by the requirements of an optimisation methodology for stator vane setting and active control of instability using controlled stator vane setting.
openaire +2 more sources