Flow studies of slender wing vortices
- 14 July 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Investigation of leading-edge devices for drag reduction of a 60-deg. delta wing at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Water tunnel flow visualization - Insight into complex three-dimensional flow fieldsaround fighter aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Strake-wing analysis and designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Prediction of Vortex Flow Characteristics of Wings at Subsonic and Supersonic SpeedsJournal of Aircraft, 1976
- Vortex development and breakdownPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- The F-12 series aircraft aerodynamic and thermodynamic design in retrospectPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Improved calculations of leading-edge separation from slender, thin, delta wingsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1968
- Vortex Breakdown Effects on the Low-speed Aerodynamic Characteristics of Slender Delta Wings in Symmetrical FlowJournal of the Royal Aeronautical Society, 1967
- Some Experiments with Vortex BreakdownJournal of the Royal Aeronautical Society, 1964