Results 101 to 110 of about 34,786 (228)

FORTRAN program for computing coordinates of circular arc single and tandem turbomachinery blade sections on a plane [PDF]

open access: yes
FORTRAN program for computing coordinates of circular arc single and tandem turbomachinery blade sections on ...
Crouse, J. E., Mc Nally, W. D.
core   +1 more source

Navier-Stokes analysis of transonic cascade flow [PDF]

open access: yes
A new kind of C-type grid is proposed, this grid is non-periodic on the wake and allows minimum skewness for cascades with high turning and large camber.
Arnone, A., Liou, M.-S., Povinelli, L.
core   +1 more source

Recent progress in inverse methods in France [PDF]

open access: yes
Given the current level of jet engine performance, improvement of the various turbomachinery components requires the use of advanced methods in aerodynamics, heat transfer, and aeromechanics.
Bry, Pierre-Francois   +2 more
core   +1 more source

NUMERICAL MODELLING OF THERMOACOUSTIC PHENOMENON AS CONTRIBUTION TO THERMOACOUSTIC ENGINE MODEL

open access: yesTASK Quarterly, 2010
The presented paper shows our first step into the numerical modelling of the thermoacoustic phenomenon. The thermoacoustic effect has a great application potential, for instance, in thermoacoustic engines or thermoacoustic mixture separation.
LESZEK REMIORZ   +2 more
doaj  

MODELLING OF INFLUENCE OF TURBULENT TRANSITION ON HEAT TRANSFER CONDITIONS

open access: yesTASK Quarterly, 2008
This article deals with the turbulent transition phenomenon modelling and its influence on heat transfer. The purpose of the analyses was to verify the transition modelling implemented in the ANSYS CFX 11 commercial code for popular test cases (low flow
KRZYSZTOF BOCHON   +2 more
doaj  

Utilization of parallel processing in solving the inviscid form of the average-passage equation system for multistage turbomachinery [PDF]

open access: yes
A procedure is outlined which utilizes parallel processing to solve the inviscid form of the average-passage equation system for multistage turbomachinery along with a description of its implementation in a FORTRAN computer code, MSTAGE.
Adamczyk, John J.   +4 more
core   +1 more source

Thermodynamic and turbomachinery concepts for radioisotope and reactor brayton-cycle space power systems [PDF]

open access: yes
Thermodynamic and turbomachinery concepts for low power radioisotope and intermediate power reactor Brayton cycle systems - examination of intercooling and reheating ...
Glassman, A. J.
core   +1 more source

A PC-based inverse design method for radial and mixed flow turbomachinery [PDF]

open access: yes
An Inverse Design Method suitable for radial and mixed flow turbomachinery is presented. The codes are based on the streamline curvature concept; therefore, it is applicable for current personal computers from the 286/287 range.
Skoe, Ivar Helge
core   +1 more source

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