Results 151 to 160 of about 18,174 (265)

Performance of a J85-13 compressor with clean and distorted inlet flow [PDF]

open access: yes
The results presented are of a series of experimental tests in which a J85-13 turbojet engine was subjected to both distorted and undistorted inlet total pressure conditions.
Milner, E. J., Wenzel, L. M.
core   +1 more source

Model equation for simulating flows in multistage turbomachinery [PDF]

open access: yes
A steady, three-dimensional average-passage equation system is derived for use in simulating multistage turbomachinery flows. These equations describe a steady, viscous flow that is periodic from blade passage to blade passage.
Adamczyk, J. J.
core   +1 more source

Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems. Task 5: Unsteady counterrotation ducted propfan analysis [PDF]

open access: yes
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.
core   +1 more source

Design of a miniature hydrogen fueled gas turbine engine [PDF]

open access: yes
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]

open access: yes
Boundary layer blowing techniques for high lift stator blades in axial flow ...
Chapman, D. C., Miller, M. L.
core   +1 more source

Performance and Stall Margin Evaluation of Axial Slot Casing Treatment in a Transonic Multistage Compressor

open access: bronze
Pedro Seiti Seiti Endo   +4 more
openalex   +2 more sources

Prediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer [PDF]

open access: yes
A method of estimating the undistorted stall line for an axial-flow compressor by using the digital computer is presented. The method involves linearization of nonlinear dynamic equations about an operating point on a speed line, and then application of ...
Blaha, R. J.   +2 more
core   +1 more source

Challenges, Opportunities and Future Directions of Membrane Technology for Natural Gas Purification: A Critical Review. [PDF]

open access: yesMembranes (Basel), 2022
Imtiaz A   +6 more
europepmc   +1 more source

Effect of slotted casing treatment on performance of a multistage compressor [PDF]

open access: yes
A J85-13 engine was equipped with a compressor case that allowed changes to the case wall over the rotor tips of six of its eight stages. The engine was tested with four inlet configurations: uniform inlet flow, 180 degree circumferential distortion, hub
Moss, J. E., Jr.
core   +1 more source

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