The effects of blunt leading edges on delta wings at Mach 5.8
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document. Pressure distributions were measured on a series of four delta wings with subsonic and supersonic leading edges, both sharp and blunt. The blunt leading edge radius was about 0.5 per c...
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Nicholson, Kenneth F. (1958) The effects of blunt leading edges on delta wings at Mach 5.8. Engineer's thesis, California Institute of Technology. doi:10.7907/ZSFZ-MN41. https://resolver.caltech.edu/CaltechETD:etd-01242006-094259 <https://resolver.caltech.edu/CaltechETD:etd-01242006-094259>