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- W1541629717 abstract "Tests utilizing the Schlieren method of flow photography have been conducted to provide a comparison of the complete flow fields past a straight and a swept-wing-body combination and the flow fields past their equivalent bodies of revolution at Mach numbers around 1.0. The results indicated that the shock growth and positions on the wing-body combinations were closely reproduced in the flow past the equivalent body." @default.
- W1541629717 created "2016-06-24" @default.
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- W1541629717 date "1956-06-01" @default.
- W1541629717 modified "2023-09-24" @default.
- W1541629717 title "The Flow past an Unswept-and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers near 1.0" @default.
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