Application of the Doublet-Lattice Method to Nonplanar Configurations in Subsonic Flow
- 1 June 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (6) , 406-413
- https://doi.org/10.2514/3.59117
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Application of oscillatory aerodynamic theory to estimation of dynamic stability derivativesJournal of Aircraft, 1970
- Correlation of the vortex lattice method on rotor/wing configurations.Journal of Aircraft, 1969
- Some New Concepts in Oscillatory Lifting Surface TheoryPublished by Defense Technical Information Center (DTIC) ,1969
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969
- Analysis and design of wing-body combinations at subsonic and supersonic speeds.Journal of Aircraft, 1968
- Numerical lifting-surface theory - Problems and progress.AIAA Journal, 1968
- Structural dynamic stability augmentation and gust alleviation of flexible aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- The Theory of Thin Wings in Subsonic FlowPublished by Springer Nature ,1967