Closed-form lift and moment for Osborne's unsteady thin-airfoil theory.
- 1 September 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (9) , 1358-1360
- https://doi.org/10.2514/3.6927
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Compressible unsteady interactions between blade rows.AIAA Journal, 1973
- Unsteady thin-airfoil theory for subsonic flow.AIAA Journal, 1973
- Finite elements for axisymmetric solids under arbitrary loadings with nodes on origin.AIAA Journal, 1972
- Application of the Matrix Displacement Method to the Analysis of Pressure VesselsJournal of Engineering for Industry, 1970
- On the Lift and Circulation of Airfoils in Some Unsteady-Flow ProblemsJournal of the Aeronautical Sciences, 1952