درباره ما
NACA-TN-1423
The stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds
Year: 1947
Abstract: The stability derivatives treated herein are listed, together with the values found for then, in table I. The derivations that follow give the values with reference to the principal body axes of figure 1 with origin at the aerodynamic center (2/3c, 0, 0). Conversion has been made to the system of stability axes shown in figure 3 with origin a distance xcg ahead of the 2/3c point (transformation equations in reference 3). Table I comprises parallel columns which present the values relative to both systems.
Subject: AIR
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:12:47Z | |
| date available | 2017-09-04T16:12:47Z | |
| date copyright | 01/01/1947 | |
| date issued | 1947 | |
| identifier other | SPTSYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/76046 | |
| description abstract | The stability derivatives treated herein are listed, together with the values found for then, in table I. The derivations that follow give the values with reference to the principal body axes of figure 1 with origin at the aerodynamic center (2/3c, 0, 0). Conversion has been made to the system of stability axes shown in figure 3 with origin a distance xcg ahead of the 2/3c point (transformation equations in reference 3). Table I comprises parallel columns which present the values relative to both systems. | |
| language | English | |
| title | NACA-TN-1423 | num |
| title | The stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds | en |
| type | standard | |
| page | 36 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1947 | |
| contenttype | fulltext | |
| subject keywords | AIR | |
| subject keywords | AIRFOILS | |
| subject keywords | ASPECT | |
| subject keywords | CALCULATIONS | |
| subject keywords | DELTA | |
| subject keywords | DIHEDRAL | |
| subject keywords | DISTRIBUTION | |
| subject keywords | FLOW | |
| subject keywords | FUSELAGES | |
| subject keywords | HIGH | |
| subject keywords | INTERFERENCE | |
| subject keywords | PRESSURE | |
| subject keywords | RATIO | |
| subject keywords | SIDESLIPPING | |
| subject keywords | SMALL | |
| subject keywords | STABILITY | |
| subject keywords | SUBSONIC | |
| subject keywords | SUPERSONIC | |
| subject keywords | THIN | |
| subject keywords | VELOCITY | |
| subject keywords | WINGS |