Numerical investigation of leading-edge vortex for low-aspect ratio thin wings
- 1 February 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (2) , 253-255
- https://doi.org/10.2514/3.7081
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Nonlinear Finite Element Analysis of Sandwich Shells of RevolutionAIAA Journal, 1973
- A Numerical Method for Calculating the Trailing Vortex System behind a Swept Wing at Low SpeedThe Aeronautical Journal, 1971
- Improved calculations of leading-edge separation from slender, thin, delta wingsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1968
- General theory of sandwich plates with dissimilar facingsInternational Journal of Solids and Structures, 1965
- Large deflection of sandwich plates with orthotropic coresAIAA Journal, 1964
- Finite Deflections of Sandwich PlatesJournal of the Aeronautical Sciences, 1948