Aerodynamic Performance of a Biplane Micro Air Vehicle
- 1 January 2007
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 44 (1) , 291-299
- https://doi.org/10.2514/1.23286
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Design of precision balance and aerodynamic characteristic measurement system for micro aerial vehiclesAerospace Science and Technology, 2006
- Effect of Tip Vortex on Wing Aerodynamics of Micro Air VehiclesJournal of Aircraft, 2005
- A Novel, Low Reynolds Number Moment Balance Design for Micro Air Vehicle ResearchPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2005
- Effects of Propulsive-Induced Flow on the Aerodynamics of Micro Air VehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2005
- Low Aspect Ratio Aerodynamics at Low Reynolds NumbersAIAA Journal, 2004
- Theoretical and Experimental Investigation of Biplane Delta WingsJournal of Aircraft, 2001
- Low Reynolds Number Aerodynamics of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate WingsJournal of Aircraft, 2000
- Multidisciplinary Design and Prototype Development of a Micro Air VehicleJournal of Aircraft, 1999