| タイトル | Forcing function effects on unsteady aerodynamic gust response. II - Low solidity airfoil row response |
| 著者（英） | Fleeter, Sanford; Henderson, Gregory H. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1992-06-01 |
| 言語 | eng |
| 内容記述 | The paper investigates the fundamental gust modeling assumption on the basis of a series of experiments performed in the Purdue Annular Cascade Research Facility. The unsteady period flow field is generated by rotating flows of perforated plates and airfoil cascades, with the resulting unsteady periodic chordwise pressure response of a downstream low solidity stator row determined by miniature pressure transducers embedded within selected airfoils. When the forcing function exhibited the characteristics of a linear-theory gust, the resulting response on the downstream stator airfoils was in excellent agreement with the linear-theory models. When the forcing function did not exhibit linear-theory gust characteristics, the resulting unsteady aerodynamic response of the downstream stators was much more complex and correlated poorly with the linear-theory gust predictions. It is shown that the forcing function generator significantly affects the resulting gust response, with the complexity of the response characteristics increasing from the perforated-plate to the airfoil-cascade forcing functions. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 93A19401
ASME PAPER 92-GT-175 |
| 権利 | Copyright |
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