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FE Modeling Methodology for Load Analysis and Preliminary Sizing of Aircraft Wing Structure

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FE Modeling Methodology for Load Analysis and Preliminary Sizing of Aircraft Wing Structure

Jun Hwan Jang et al · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793

It is a critical part at the basic design phase of aircraft structural design to build a finite element model and it will have a direct impact on time and cost for airframe structure development. In addition, the objecti...

LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng

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Design and Realization of an Unmanned Aerial Rotorcraft Vehicle Using Pressurized Inflatable Structure

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Design and Realization of an Unmanned Aerial Rotorcraft Vehicle Using Pressurized Inflatable Structure

Nirmal Sadasivan · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793

Unmanned aerial rotorcraft vehicles have many military, commercial and civil applications. There is a necessity to advance the performance on several ranges of rotorcraft for using these vehicles successfully in the expa...

LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng

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