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  1. blondefletch

    Removable Stressed Skin Fuselage Panelling

    Meant to put in aero-structures for KENAT, apologies. Either way, thanks for your input
  2. blondefletch

    Removable Stressed Skin Fuselage Panelling

    Thank you all very much for your comments. Greg, the image I used was a patented design, in which I thought exactly the same as you. Good to get a technical peer appraisal, so thanks again. KENAT, regardless of the non-aero background, very useful stuff once again, thanks. I'll be pursuing a...
  3. blondefletch

    Removable Stressed Skin Fuselage Panelling

    Hi Kenat, To clarify, this is a project based completely in my spare time, with the question more related to future projects. Thanks for your response, it is solely structural considerations, just trying to prompt a discussion on what methods can be used to make stressed skin panels removable...
  4. blondefletch

    Removable Stressed Skin Fuselage Panelling

    Hi folks, I'm currently undertaking a fuselage design project for a UAV. My question relates to something I read in this textbook, link to paragraph: Unmanned Aircraft Systems: UAVS Design, Development and Deployment by Reg Austin (http://bit.ly/zMaMaK). I am looking at potential design...
  5. blondefletch

    Help - Finding external wetted area of a single boundary surface

    Hi, Need to measure the external surface area of a boundary surface for CFD analysis. Any way of doing this in Solidworks 2010? Aware of methods for the entire model, but not for individual bits. Its a fuselage, screenshot attached, need to find the surface area of the entire fuselage. Any...

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