Using helium hypersonic wind tunnel, exploratory studies are made of flow over simple 2- and 3-dimensional bodies at Mach numbers from 11 to 19; studies of flow over flat plate and preliminary results for other configurations, including flat plates with flaps, delta wings, base pressure models, blunt models and slim cones; some preliminary results of boundary layer studies and dissolving models.
Exploratory studies of hypersonic fluid mechanics
AGARD Report
AGARD -- Report ; n 142
1957
30 pages
Report
Englisch
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