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- W2026216338 abstract "Scale model compressed air tests of 260-inch solid rocket with submerged nozzle to determine exhaust flow velocity and direction in annular channel" @default.
- W2026216338 created "2016-06-24" @default.
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- W2026216338 date "1967-06-06" @default.
- W2026216338 modified "2023-09-24" @default.
- W2026216338 title "INVESTIGATION OF A SUBMERGED NOZZLE FOR SOLID ROCKETS" @default.
- W2026216338 doi "https://doi.org/10.2514/6.1967-1520" @default.
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