Increasing the Lift-Drag Ratio of an Unmanned Aerial VehicleUusing Local Twist
- 1 January 2008
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 45 (1) , 10-15
- https://doi.org/10.2514/1.33353
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Minimizing Induced Drag with Wing Twist, Computational-Fluid-Dynamics ValidationJournal of Aircraft, 2006
- Comparison of Unsteady Aerodynamic Modelling Methodologies with Respect to Flight Loads AnalysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2005
- Design of an Unmanned Aerial Vehicle for Ecological ConservationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2005
- Lifting-Line Analysis of Roll Control and Variable TwistJournal of Aircraft, 2004
- Lifting-Line Analysis for Twisted Wings and Washout-Optimized WingsJournal of Aircraft, 2004
- Low-Speed AerodynamicsPublished by Cambridge University Press (CUP) ,2001
- Flight test of a half-scale unmanned air vehicleJournal of Aircraft, 1991