naca-rm-a57a10
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- October 9, 2017 Create Date
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National Advisory Committee for Aeronautics, Research Memorandum - A Wind Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration having a Triangular Wing of Aspect Ratio 2.2
| File | Action |
|---|---|
| naca-rm-a57a10 A Wind Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration hacing a Triangular Wing of.pdf | Download |
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