Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Dana A. Gottfried"'
Publikováno v:
Journal of Propulsion and Power. 26:16-24
A mathematical model is developed to investigate the effects of aerodynamic damping on the maximum amplification factor of mistuned bladed disks. LINSUB, an inviscid linearized unsteady aerodynamic damping code, provides aerodynamic damping influence
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bb14f8ba4151931148b7186ab32d2818
https://doi.org/10.2514/1.36537
https://doi.org/10.2514/1.36537
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
Autor:
Sanford Fleeter, Dana A. Gottfried
Publikováno v:
Journal of Propulsion and Power. 21:327-334
Flow-induced vibration of turbomachine blade rows is a coupled fluid-structure problem. Thus, rather than separate fluid and structural models, a coupled interacting fluid-structures analysis is needed. This need is addressed by extending the finite
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bdb3989aff5ea0f68f49bf1973eaa77c
https://doi.org/10.2514/1.4720
https://doi.org/10.2514/1.4720
Autor:
Dana A. Gottfried, Sanford Fleeter
Publikováno v:
Journal of Propulsion and Power. 18:978-989
High-cycle fatigue (HCF) is a key issue for the advancement of gas-turbine performance and endurance. Models simulating the cyclic aerodynamic forces experienced by gas-turbine vanes are necessary to make quantitative predictions of HCF during design
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8f50bed1c64704ca1580570ef2b1e995
https://doi.org/10.2514/2.6044
https://doi.org/10.2514/2.6044
Autor:
Sanford Fleeter, Dana A. Gottfried
Publikováno v:
Journal of Propulsion and Power. 18:472-480
To predict the unsteady aerodynamic response of centrifugal compressor impeller blades to the potential field generated by the downstream vaned diffuser, a small perturbation model is developed that considers the number of impeller blades and diffuse
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f520db576679663eaeba3a73bb2c08ef
https://doi.org/10.2514/2.5958
https://doi.org/10.2514/2.5958
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
High Cycle Fatigue (HCF) is a key issue in the development and endurance of gas turbine engines that results from the flow-induced vibratory response of turbomachine blading to unsteady aerodynamic excitations. This paper describes the development an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e48440d825913bb2770ba3295de006fc
https://doi.org/10.2514/6.2006-627
https://doi.org/10.2514/6.2006-627
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::53d85860d631e6e7b429f7509bdc1a8e
https://doi.org/10.2514/6.2002-3639
https://doi.org/10.2514/6.2002-3639
Autor:
Dana A. Gottfried, Sanford Fleeter
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Geometric detuning effects are considered in this study of flow induced vibrations of the I nlet Guide Vane (IGV) row of the Purdue Transonic Compressor. The TAM -ALE3D fluid -structure interaction finite element code is used for the analysis, with t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e5596dd1995eb720c6c476f3019d5667
https://doi.org/10.2514/6.2002-3634
https://doi.org/10.2514/6.2002-3634
Autor:
Sanford Fleeter, Dana A. Gottfried
Publikováno v:
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
High cycle fatigue (HCF) i s a key issue for the advancement of gas turbine performance and endurance. TAM -ALE3D, a model that simulates cyclic aerodynamic forces and internal blading stresses, is evaluated at off -design conditions where aerodynami
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0ed52eda66e27ae3ac772576a4ecade8
https://doi.org/10.2514/6.2002-4219
https://doi.org/10.2514/6.2002-4219
Autor:
Dana A. Gottfried, Sanford Fleeter
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
Flow induced vibration of turbomachine blade rows is a coupled fluid-structure problem. Thus, rather than separate fluid and structural models, a coupled interacting fluid-structures analysis is needed. This research addresses this need by extending
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::afb8ec1eb2cb1e7d80e12fd06d1b037b
https://doi.org/10.2514/6.1999-2810
https://doi.org/10.2514/6.1999-2810