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NACA-TN-2699
Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges
Year: 1952
Abstract: On the basis of linearized supersonic-flow theory the stability derivatives Cma and Cmq (moment coefficients due to angle of attack and steady pitching velocity, respectively) and CLq (lift coefficient due to steady pitching velocity) were derived for a series of thin sweptback tapered wings with stream wise tips and supersonic leading and trailing edges. The results are valid for a range of Mach number for which the Mach lines from the-leading edge of the center section cut the trailing edges. An additional limitation is that the foremost Mach line from either tip may not intersect the remote half of the wing.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:16:06Z | |
| date available | 2017-09-04T15:16:06Z | |
| date copyright | 01/01/1952 | |
| date issued | 1952 | |
| identifier other | MILUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/15240 | |
| description abstract | On the basis of linearized supersonic-flow theory the stability derivatives Cma and Cmq (moment coefficients due to angle of attack and steady pitching velocity, respectively) and CLq (lift coefficient due to steady pitching velocity) were derived for a series of thin sweptback tapered wings with stream wise tips and supersonic leading and trailing edges. The results are valid for a range of Mach number for which the Mach lines from the-leading edge of the center section cut the trailing edges. An additional limitation is that the foremost Mach line from either tip may not intersect the remote half of the wing. | |
| language | English | |
| title | NACA-TN-2699 | num |
| title | Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges | en |
| type | standard | |
| page | 117 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1952 | |
| contenttype | fulltext |