1,721,204 research outputs found
Design of Hat-stiffened composite panels under uniaxial compression and shear - minimum mass optimization based on a simplified theory
Aerospace Engineerin
Manufacturing and Testing of Graphite-Epoxy Wing Box and Fuselage Structures for a Solarpowered UAV-HAVE
Analytical and Experimental Results of Integral Composite Panels Subjected to Compression and Shear. (Risultati teorico-sperimentali di pannelli integrali in materiale composito soggetti a compressione e taglio)
"Identification of Requirements for an Aircraft in Selected Category"
Deliverable D6/2, ENFICA-F
"Initial Design Effort in Conversion of chosen Aircraft into Electric-Motor-Driven Airplane"
Deliverable D6/3, ENFICA-F
Analytical and experimental behaviour of anisotropic panels subjected to linearly varying biaxial compression and shear loads
Design, Realization & flight Tests of a 2-Seats Aircraft powered by Hydrogen fuel cell electric propulsion. - Fuel Cells & Solar Cells Long Endurance UAV
Invited lectures of ARGENTINA Ministerio de Ciencia, Tecnologia e Innovacion Productiva. Cordoba, INVAP, 7 Nov 2011. Istituto de Aeronautica, 8 Nov 2011. Univ. Nacional de Catamarca, 9 Nov. 201
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