Aerodynamic design, analysis and testing of propellers for small unmanned aerial vehicles

AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting

Volumn , Issue , 2017, Pages

  Anemaat, Willem A J ^a   Schuurman, Menco ^a   Liu, Wanbo ^a   Karwas, Alex ^a  

^a Design Analysis and Research Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85017254770     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2017-0721     Document Type: Conference Paper

References (8)

1. Treggon Owens, UAS Set to Transform Aerospace and the World, Keynote Speech at AIAA SCITECH 2013, January 4-8, 2016, San Diego, California.
2. Biermann, David and Hartman, Edwin P., The Aerodynamic Characteristics of Full-Scale Propellers Having 2, 3 and 4 Blades of Clark Y and R.A.F. 6 Airfoil Sections, NACA Report No. 640., NACA-TR-640, January 1938.
3. PropellerScanner, MH AeroTools, Braunshweig, Germany, Version 1.1.
4. STAR-CCM+, Version 10.04.011, Computational Dynamics-Analysis & Design Application Co., Ltd. (CD-adapco), Melville, New York, 2015.
5. Drzewiecki, S., Theorie Generale de l‘Helice, Gauthiers-Villars et Cie, 1920.
6. Stepniewski, W.Z. and Keys, C.N., Rotary-Wing Aerodynamics, Dover.
7. Siemens Femap and NX Nastran Software Package, Version 11.0, Siemens PLM Software, Plano, Texas, 2013.
8. NATO Standardization Agency, UAV Systems Airworthiness Requirements (USAR) for North Atlantic Treaty Organization (NATO) Military UAV Systems, STANAG 4671, Edition 1, 2009, Brussels, Belgium.