naca-tn-1659
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- December 4, 2016 Create Date
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National Advisory Committee for Aeronautics, Technical Notes - Method for Calculation of Pressure Distributions on Thin Conical Bodies of Arbitrary Cross Section in Supersonic Stream
| File | Action |
|---|---|
| naca-tn-1659 Method for Calculation of Pressure Distributions on Thin Conical Bodies of Arbitrary Cross Section in Supersonic Stream.pdf | Download |
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