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NACA-RM-L54C16
Experimental effects of propulsive jets and afterbody configurations on the zero-lift drag of bodies of revolution at a Mach number of 1.59
Year: 1954
Abstract: The present investigation was made at a free-stream Mach number of 1.59 to compare the afterbody drags to a series of conical boattailed models at zero angle of attack. Afterbody drags were obtained for both the power-off and the power-on conditions. Power-on drags were obtained as a function of afterbody fineness ratio, jet pressure ratio and divergence, and jet Mach number.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:07:44Z | |
| date available | 2017-09-04T18:07:44Z | |
| date copyright | 01/01/1954 | |
| date issued | 1954 | |
| identifier other | GPSWXDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/190670 | |
| description abstract | The present investigation was made at a free-stream Mach number of 1.59 to compare the afterbody drags to a series of conical boattailed models at zero angle of attack. Afterbody drags were obtained for both the power-off and the power-on conditions. Power-on drags were obtained as a function of afterbody fineness ratio, jet pressure ratio and divergence, and jet Mach number. | |
| language | English | |
| title | NACA-RM-L54C16 | num |
| title | Experimental effects of propulsive jets and afterbody configurations on the zero-lift drag of bodies of revolution at a Mach number of 1.59 | en |
| type | standard | |
| page | 34 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1954 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | ANGLE | |
| subject keywords | ANGLES | |
| subject keywords | ATTACK | |
| subject keywords | BASE | |
| subject keywords | BOATTAILS | |
| subject keywords | BODIES | |
| subject keywords | CONICAL | |
| subject keywords | DISTRIBUTION | |
| subject keywords | DRAG | |
| subject keywords | EXHAUST | |
| subject keywords | FLOW | |
| subject keywords | FREE | |
| subject keywords | GEOMETRY | |
| subject keywords | INTERFERENCE | |
| subject keywords | JET | |
| subject keywords | LIFT | |
| subject keywords | MACH | |
| subject keywords | NOZZLES | |
| subject keywords | NUMBER | |
| subject keywords | PRESSURE | |
| subject keywords | RATIO | |
| subject keywords | REVOLUTION | |
| subject keywords | ZERO |