Zobrazeno 1 - 10
of 10
pro vyhledávání: '"F. O. Carta"'
Publikováno v:
Journal of Turbomachinery. 113:219-225
The fluid dynamics of turbomachines are extremely complex, due in part to the aerodynamic interactions between rotors and stators. It is necessary to acquire fluid dynamic data that reflect the interactive nature of a turbomachine to correlate with t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::618322304659e65d550c714e861e83dc
https://doi.org/10.1115/1.2929087
https://doi.org/10.1115/1.2929087
Publikováno v:
Journal of Turbomachinery. 113:226-226
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d79e3b557701c32b34ab4e3b54bd840a
https://doi.org/10.1115/1.2929089
https://doi.org/10.1115/1.2929089
Autor:
F. O. Carta, G. L. Commerford
Publikováno v:
AIAA Journal. 12:43-48
An experimental technique is described which corroborates the predictions of several new analyses of the unsteady response of an airfoil to high frequency flow fluctuations. The periodically fluctuating flowfield was produced by the natural shedding
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c2bae32cd0c0c91c91a27bde7924f156
https://doi.org/10.2514/3.49151
https://doi.org/10.2514/3.49151
Publikováno v:
Journal of Turbomachinery. 109:499-507
An experiment was conducted on a heavily instrumented isolated model compressor rotor to study the unsteady aerodynamic response of the blade row to a controlled pitching oscillation of all blades in an undistorted flow, and to a circumferential inle
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d74b0b53d848a1cfa627f616da0f363c
https://doi.org/10.1115/1.3262139
https://doi.org/10.1115/1.3262139
Autor:
F. O. Carta, A. O. St. Hilaire
Publikováno v:
Journal of Engineering for Power. 100:111-120
Tests were performed on a linear cascade of airfoils oscillating in pitch about their midchords at frequencies up to 17 cps, at free-stream velocities up to 200 ft/s, and at interblade phase angles of 0 deg and 45 deg, under conditions of high aerody
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b9863da6f082598748687ba8750b8f5
https://doi.org/10.1115/1.3446301
https://doi.org/10.1115/1.3446301
Autor:
F. O. Carta
Publikováno v:
Journal of Engineering for Power. 105:565-574
Tests were conducted on a linear cascade of airfoils oscillating in pitch to measure the unsteady pressure response on selected blades along the leading edge plane of the cascade and over the chord of the center blade. The pressure data were reduced
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81036d48dac2555e2d739d9457f99835
https://doi.org/10.1115/1.3227455
https://doi.org/10.1115/1.3227455
Autor:
F. O. Carta
Publikováno v:
Journal of Engineering for Power. 89:419-426
An energy method is used to investigate a flutter instability of turbojet engine rotors which is caused by the interactions between unsteady air loading and the coupled vibration modes of the rotating blade-disk-shroud system. It is shown, analytical
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::70265625daaa1d1a77c738ca47fed1de
https://doi.org/10.1115/1.3616708
https://doi.org/10.1115/1.3616708
Autor:
F. O. Carta
Publikováno v:
Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; Process Industries; Technology Resources; General.
Tests were conducted on a linear cascade of airfoils oscillating in pitch to measure the unsteady pressure response on selected blades along the leading edge plane of the cascade and over the chord of the center blade. The pressure data were reduced
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7fd966544f825beb0b012be520f918d
https://doi.org/10.1115/82-gt-286
https://doi.org/10.1115/82-gt-286
Autor:
F. O. Carta
Publikováno v:
13th Aerospace Sciences Meeting.
The dynamic stall phenomenon was examined in detail by analyzing a set of unsteady pressure data obtained on an airfoil oscillating in pitch. These data were for sinusoidal oscillations which penetrated the stall region in varying degrees, and here t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f626854f6782296c499c2ad5020c6099
https://doi.org/10.2514/6.1975-25
https://doi.org/10.2514/6.1975-25
Autor:
F. O. Carta
Publikováno v:
Journal of Engineering for Industry. 89:680-681
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3ff68ede53d437fefca366dc2b596970
https://doi.org/10.1115/1.3610132
https://doi.org/10.1115/1.3610132