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Program for impact testing of spar-shell fan blades, test report (1978)

Ravenhall, R. ; Salemme, C. T.

In: CASI

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Publication Date: 2019-06-27

Description: Six filament-wound, composite spar-shell fan blades were impact tested in a whirligig relative to foreign object damage resulting from ingestion of birds into the fan blades of a QCSEE-type engine. Four of the blades were tested by injecting a simulated two pound bird into the path of the rotating blade and two were tested by injecting a starling into the path of the blade.

Keywords: AIRCRAFT PROPULSION AND POWER

Type: NASA-CR-135393 , R78AEG444

Format: application/pdf

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