NASA NTRS · 19720009558
Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small-disturbance equations, part 2
Abstract
For abstract, see N72-17207.
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Dsylva, E.. 1972-02-01. Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small-disturbance equations, part 2. https://ntrs.nasa.gov/citations/19720009558
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