Cylinder/Splitter-Plate Data Illustrating High a Support Interference
- 1 March 1979
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 16 (2) , 126-128
- https://doi.org/10.2514/3.57631
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Experimental investigation of support interference on an ogive cylinder at high incidencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- The effects of wake splitter plates on bluff-body flow in the range 104 < R < 5 × 104. Part 2Journal of Fluid Mechanics, 1975
- The effects of wake splitter plates on the flow past a circular cylinder in the range 104<R4Journal of Fluid Mechanics, 1973
- The mechanics of the formation region of vortices behind bluff bodiesJournal of Fluid Mechanics, 1966
- Investigation of the flow behind a two-dimensional model with a blunt trailing edge and fitted with splitter platesJournal of Fluid Mechanics, 1965