Hover Performance of a Micro Air Vehicle: Rotors at Low Reynolds Number
- 1 July 2007
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 52 (3), 254-262
- https://doi.org/10.4050/jahs.52.254
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Design, Analysis and Hover Performance of a Rotary Wing Micro Air VehicleJournal of the American Helicopter Society, 2003
- High Resolution Trailing Vortex Measurements in the Wake of a Hovering RotorJournal of the American Helicopter Society, 2003
- Comparison of Wing Characteristics at an Ultralow Reynolds NumberJournal of Aircraft, 2002
- Wind tunnel tests of wings at Reynolds numbers below 70 000Experiments in Fluids, 1997