WISDOMProject reference: 325978
Funded under :
WING STRUCTURAL TEST DEVELOPMENT METHOD
Total cost:EUR 3 430 272
EU contribution:EUR 2 572 704
Topic(s):JTI-CS-2012-2-SFWA-03-010 - BLADE wing structural test to derive test data for subsequent validation of GFEM modelling
Call for proposal:SP1-JTI-CS-2012-02See other projects for this call
Funding scheme:JTI-CS - Joint Technology Initiatives - Clean Sky
"The proposal approach innovative solutions for the design and manufacturing of the test rig and the definition of the method and prformance for the structural testing of two different kinds of configuration for the outer wings within a Smart Fixed Wing Aircraft.
The WISDOM proposal, understand that the test philosophy is to demonstrate that major components tests can be performed on flight test aircraft.
The main requirement for this wing structural part is based on their high dimensional stability and tight geometrical tolerances to compliance with surface quality for a natural laminar flow condition, and therefore stability control and manufacturing precision over the test bench tools to be designed and manufactured shall consider this, avoiding as much as possible interfaces with the specimen surfaces.
The test procedure is based in a Self-supporting test rig with flexible and adaptative plug and play loads introduction method with minimum specimen interface needs and wireless connection for data recording"
EU contribution: EUR 1 561 644
RITA LEVI MONTALCINI 14
28906 GETAFE MADRID
EU contribution: EUR 588 960
Parque Tecnologico de Alava (Minano), C/ Juan de la Cierva 1
01510 MINANO (ALAVA)
EU contribution: EUR 422 100
CALLE WILBURG Y ORVILLE WRIGHT 1
41309 LA RINCONADA SEVILLA