Some Recent Developments in Airfoil Theory
- 1 May 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (5) , 490-499
- https://doi.org/10.2514/8.3588
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Propagation of Stall in a Compressor Blade RowJournal of the Aeronautical Sciences, 1955
- General Theory of High Speed AerodynamicsPublished by Walter de Gruyter GmbH ,1954
- The lift and moment acting on a thick aerofoil in unsteady motionPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1954
- Prediction of the Characteristics of Two-Dimensional AirfoilsJournal of the Aeronautical Sciences, 1954
- Remarks on Nonlinear Lift and Vortex SeparationJournal of the Aeronautical Sciences, 1954
- Leading-Edge Separation from Delta Wings at Supersonic SpeedsJournal of the Aeronautical Sciences, 1953
- Aerodynamic Hysteresis as a Factor in Critical Flutter Speed of Compressor Blades at Stalling ConditionsJournal of the Aeronautical Sciences, 1949
- A new treatment of the lifting-line wing theory, with applications to rigid and elastic wingsQuarterly of Applied Mathematics, 1948
- Lifting-line theory for a wing in non-uniform flowQuarterly of Applied Mathematics, 1945
- The theoretical determination of the lift coefficient for a thin elliptic cylinderProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1935