タイトル | Effect of a simulated wing on the pressure-drag coefficients of various 15 deg boattails at Mach numbers from 0.56 to 1.00 |
本文(外部サイト) | http://hdl.handle.net/2060/19680026200 |
著者(英) | Shrewsbury, G. D. |
著者所属(英) | NASA Lewis Research Center |
発行日 | 1968-10-01 |
言語 | eng |
内容記述 | Simulated wing effect on pressure drag coefficient of subsonic boattail at angle of attack |
NASA分類 | AERODYNAMICS |
レポートNO | 68N35672 NASA-TM-X-1662 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/211205 |