Zobrazeno 1 - 10
of 60
pro vyhledávání: '"Patrick B. Lawless"'
Publikováno v:
Turbomachinery Fluid Dynamics and Heat Transfer ISBN: 9780203734919
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::11f2f367f7a6086b244df90db478d7d9
https://doi.org/10.1201/9780203734919-18
https://doi.org/10.1201/9780203734919-18
Publikováno v:
Journal of Propulsion and Power. 27:296-305
The future of small gas turbines relies on higher-efficiency and higher-pressure-ratio centrifugal compressors for lighter, more efficient, and reliable designs. An efficient diffuser is essential to the performance, durability, and operability of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9809072feb65bd0270405beccb66f58e
https://doi.org/10.2514/1.45697
https://doi.org/10.2514/1.45697
Publikováno v:
Journal of Propulsion and Power. 26:784-789
High-density instantaneous and rotor phase-locked velocity field measurements are made in the centrifugal compressor diffuser vaneless space by means of the particle image velocimetry technique. The technique is challenged in this application by a sm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::68143f761e63f6706970710ac5c72318
https://doi.org/10.2514/1.38663
https://doi.org/10.2514/1.38663
Publikováno v:
Journal of Propulsion and Power. 25:642-652
This paper describes the development and application of turbomachinery aeromechanics arbitrary Lagrangian Eulerian 3-D, an arbitrary Lagrangian Eulerian finite-element-coupled fluid―structure interaction solver, to axial and radial flow turbomachin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd2ee76ea86e8a960f0c015826d150f7
https://doi.org/10.2514/1.36068
https://doi.org/10.2514/1.36068
Publikováno v:
Journal of Propulsion and Power. 23:212-220
DOI: 10.2514/1.17187 A fluid-structure interaction analysis is developed to study wake-generated turbomachine blade row unsteady aerodynamics and to predict the resulting vibratory stress. This is accomplished by incorporating the Baldwin– Lomax tu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9f07158d22d8b1b9aa5f185920724450
https://doi.org/10.2514/1.17187
https://doi.org/10.2514/1.17187
Publikováno v:
Journal of Propulsion and Power. 21:715-727
The unsteady aerodynamic interactions of a transonic rotor with an upstream inlet guide vane (IGV) row under off-design operating conditions are investigated. The rotor-generated IGV unsteady aerodynamics are quantified when the IGV reset angle cause
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d54b3812f5f509e4a91a533678a5260
https://doi.org/10.2514/1.6315
https://doi.org/10.2514/1.6315
Publikováno v:
Journal of Propulsion and Power. 20:835-841
Blade row interaction effects on airfoil unsteady aerodynamics are investigated, particularly at off-design operating conditions. The specific problem addressed is off-design unsteady aerodynamics including dynamic stall due to the interaction of rot
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e2d17173e001e1a184c9ecffd1518504
https://doi.org/10.2514/1.3878
https://doi.org/10.2514/1.3878
Publikováno v:
Journal of Propulsion and Power. 20:842-848
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::94e57bf509d7bc82f60918df32384a6c
https://doi.org/10.2514/1.3883
https://doi.org/10.2514/1.3883
Publikováno v:
Journal of Aerospace Engineering. 17:106-112
Quasi-steady instability initiation studies do not model the actual operation of a compressor in an installed engine. Namely, gas turbine engine compressors are subject to transient operation. To provide needed high-speed centrifugal compressor insta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::577f7649700c0b707ea0480841495e50
https://doi.org/10.1061/(asce)0893-1321(2004)17:3(106)
https://doi.org/10.1061/(asce)0893-1321(2004)17:3(106)
Publikováno v:
Journal of Propulsion and Power. 18:1012-1018
An experimental study is performed to characterize the behavior of a high-speed centrifugal compressor as it approaches instability. To achieve this, data at the inlet and exit of the centrifugal compressor are analyzed. Three inducer bleed condition
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0e2f6d0ea1df170e06d19dfa6a1f57a7
https://doi.org/10.2514/2.6049
https://doi.org/10.2514/2.6049