Power Requirements for Large-Amplitude Flapping Flight
- 1 May 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 35 (3) , 352-361
- https://doi.org/10.2514/2.2324
Abstract
No abstract availableThis publication has 20 references indexed in Scilit:
- Minimum induced power requirements for flapping flightJournal of Fluid Mechanics, 1996
- Helicopter rotor lift distributions for minimum-induced power lossJournal of Aircraft, 1994
- On aerodynamics and the energetics of vertebrate flapping flightContemporary Mathematics, 1993
- Unsteady lifting-line theory by the method of matched asymptotic expansionsJournal of Fluid Mechanics, 1988
- Vortex flow visualizations reveal change in upstroke function with flight speed in batsNature, 1986
- Unsteady lifting-line theory as a singular perturbation problemJournal of Fluid Mechanics, 1985
- An unsteady lifting line theory of flapping wings with application to the forward flight of birdsJournal of Fluid Mechanics, 1981
- The unsteady quasi-vortex-lattice method with applications to animal propulsionJournal of Fluid Mechanics, 1979
- A vortex theory of animal flight. Part 2. The forward flight of birdsJournal of Fluid Mechanics, 1979
- On the vortex theory of screw propellersProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1929