| タイトル | Forces and Moments on Pointed Blunt-nosed Bodies of Revolution at Mach Numbers from 2.75 to 5.00 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930087189 |
| 著者（英） | Dennis, David H; Cunningham, Bernard E |
| 著者所属（英） | National Advisory Committee for Aeronautics. Ames Aeronautical Lab. |
| 発行日 | 1952-08-08 |
| 言語 | eng |
| 内容記述 | Results of tests to determine the aerodynamic forces and moments on bodies of revolution at angles of attack from 0 degrees to 25 degrees are presented and compared with theory. Cones and ogives of fineness ratios 3 to 7 and two blunt-nosed body shapes with fineness ratios 3 and 5 were tested at Mach numbers from 2.75 to 5.00. Reynolds numbers were from 0.5 million to 6.4 million, depending on Mach number and body fineness ratio. |
| レポートNO | 93R16479
NACA-RM-A52E22 |
| 権利 | No Copyright |
