Measurements on a delta wing in unsteady flow
- 1 June 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (6) , 547-552
- https://doi.org/10.2514/3.44611
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- New smoke generator for flow visualization in low speed wind tunnelsJournal of Aircraft, 1976
- Some Measurements on Dynamic StallJournal of Aircraft, 1974
- Extension of a Vortex-Lattice Method to Include the Effects ofLeading-Edge SeparationJournal of Aircraft, 1974
- A Wind-Tunnel Stream Oscillation ApparatusJournal of Aircraft, 1972
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- On the Breakdown at High Incidences of the Leading Edge Vortices on Delta WingsJournal of the Royal Aeronautical Society, 1960