NASA NTRS · 19710018889
Numerical solutions for the complete shock wave structure behind supersonic edge delta wings
Abstract
Computerized simulation of shock waves and flow fields behind supersonic edge delta wings and wing-body combinations
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Kutler, P., Lomax, H.. 1971-01-01. Numerical solutions for the complete shock wave structure behind supersonic edge delta wings. https://ntrs.nasa.gov/citations/19710018889
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