![]() For ease of use the next time, make a shortcut to the scripts folder on your desktop. This is a hidden folder, to navigate to it, press and hold the Alt key and pull down the “Go” menu, you will see “Library” - navigate to the Scripts folder along the above path from there. ~/Library/Application Support/McNeel/Rhinoceros/Scripts Here’s how to install a script in Mac Rhino and set it up to run from an alias:ĭownload the script file and move it to the following folder: Separate release notesĪre included with the Volume 1 and Volume 2 datasets.As far as running it in Mac Rhino, the easiest way is via an alias. 11/29/15 - Started these release notes.11/29/15 - Added a link to download the entire database as a zip file.8/25/20 - Added Volume 3 dataset and updated the zip file with the entire database.4/11/22 - On this main page, gave definition of Re used in the.6/27/22 - Added Volume 4 dataset and updated the zip file with the entire database.University of Illinois at Urbana-Champaign, Illinois, Thesis, Department of Aerospace Engineering, B., "Small-Scale Propeller Performance at Low Sciences Meeting, AIAA Paper 2011-1255, Orlando, FL, and Selig, M.S., "Propeller Performance Data at Low R.W., Ananda, G.K., and Selig, M.S., "Reynolds Number EffectsĪeronautics Forum and Exposition (Aviation 2014), AIAA Dissertation, Department of AerospaceĮngineering, University of Illinois at Urbana-Champaign, Urbana, Deters, R.W., "Performance and SlipstreamĬharacteristic of Small-Scale Propellers at Low Reynolds.Gregory, J.W., private communications, June 2015.Modeling for Low- Re Small UAS Electric Propulsion Systems,"ĪIAA Aviation and Aeronautics Forum and Exposition (AviationĢ015), AIAA Paper 2015-3296, Dallas, TX, June and Gregory, J.W., "Blade Element Momentum University of Illinois at Urbana-Champaign,Ĭaccamo, C., Deters, R.W., and Selig, M.S., "Performance Testing of APC Electric Fixed-Blade UAV Propellers," AIAA Aviation and Aeronautics Forum and Exposition (Aviation 2022), AIAA Paper 2022-4020, Chicago, IL, June 2022.Ĭaccamo, C., Deters, R.W., and Selig, M.S., "Performance Testing of Aero-Naut CAM Folding Propellers," AIAA Aviation and Aeronautics Forum and Exposition (Aviation 2020), AIAA Paper 2020-2760, Virtual Event, June 2020. Selig (insert date downloaded), UIUC Propeller The recommended way to cite this webpage in a publication is: For the OSU data, the measurements were taken usingĪ multi-axis load cell attached directly to the motor (Ref 8).ĪPC 10x5E and 10x7E "thin electric" propellers.Ĭredits: Graphics provided by Matthew McCrink and James Gregory, ![]() Torque is measured through a torque cell attached to the fixture that Measured directly with a load cell attached to a pivot arm. The results show goodĪgreement, especially considering that the thrust and torque UIUC and Ohio State University Experimental Measurements - Comparisonĭata and measurements taken at Ohio State (Ref 6). The extension to ".txt" allows for the files to be easily opened in any The file to obtain is: PE0-FILES_WEB-202206.zipx (or latest). Geometry information direct from APC is here: Many of the propellers tested are APC brand propellers. "Aerodynamics, Aeronautics, and Flight Mechanics," Quantities at the 75% blade station: propeller blade chord (c_75%)Īnd rotational velocity (V_75% = 0.75 Ω R).įor more information, a useful reference is: Reynolds number reported there (x-axis) is based on these The UIUC data use the standard definitions for propeller aerodynamic coefficients:įurther, for the static performance data plots (C_T0, C_P0), the Volume 4 - Publication and tests by Or Dantsker (2021-2022).Volume 3 - Publication and tests by Or Dantsker (2020).Last updated 2/3/15ĭissertation by Robert Deters and following tests (2009-2015). ![]() Thesis by John Brandt and following tests The propeller database includes three volumes: This webpage includes wind tunnel measurements for propellers used
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