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Performance of two-stage fan with larger dampers on first-stage rotor (1979)

Cunnan, W. S. ; Urasek, D. C. ; Stevans, W.

In: CASI

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Publication Date: 2019-06-27

Description: The performance of a two stage, high pressure-ratio fan, having large, part-span vibration dampers on the first stage rotor is presented and compared with an identical aerodynamically designed fan having smaller dampers. Comparisons of the data for the two damper configurations show that with increased damper size: (1) very high losses in the damper region reduced overall efficiency of first stage rotor by approximately 3 points, (2) the overall performance of each blade row, downstream of the damper was not significantly altered, although appreciable differences in the radial distributions of various performance parameters were noted, and (3) the lower performance of the first stage rotor decreased the overall fan efficiency more than 1 percentage point.

Keywords: AIRCRAFT PROPULSION AND POWER

Type: NASA-TP-1399 , E-8958

Format: application/pdf

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