In this report the conditions that will be used for the aircraft ditching tests to be performed at CNR- INSEAN are presented. According to what planned in the original proposal and subsequent discussions within the consortium, four different test typologies will be considered, which correspond to the four tasks of the WP5. Namely they will be conducted on: double curvature rigid specimen, single curvature aircraft-like structure, thin flat plates and scaled fuselage with dynamic pitch. The main features of the shapes and of the structures to be used in the test campaign as well as some aspects concerning with the instrumentation are provided together with the test matrix.
D5.1: Definition of the conditions for guided aircraft ditching tests
Alessandro Iafrati;Flavio Olivieri
2017
Abstract
In this report the conditions that will be used for the aircraft ditching tests to be performed at CNR- INSEAN are presented. According to what planned in the original proposal and subsequent discussions within the consortium, four different test typologies will be considered, which correspond to the four tasks of the WP5. Namely they will be conducted on: double curvature rigid specimen, single curvature aircraft-like structure, thin flat plates and scaled fuselage with dynamic pitch. The main features of the shapes and of the structures to be used in the test campaign as well as some aspects concerning with the instrumentation are provided together with the test matrix.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
