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NACA-ARR-L5F23
Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces
Year: 1945
Abstract: INTRODUCTION
One of the many aerodynamic problems for which a theoretical solution by means of lifting-line theory might be expected to be inadequate is the case of a wing in steady roll. Robert T. Jones has obtained in an unpublished analysis similar to that of reference 1 a correction to the lifting-line-theory values of the damping in roll that amounts to an B-percent reduction in the values for a wing of aspect ratio 6. Still more accurate values may be obtained by use of lifting-surface theory.
One of the many aerodynamic problems for which a theoretical solution by means of lifting-line theory might be expected to be inadequate is the case of a wing in steady roll. Robert T. Jones has obtained in an unpublished analysis similar to that of reference 1 a correction to the lifting-line-theory values of the damping in roll that amounts to an B-percent reduction in the values for a wing of aspect ratio 6. Still more accurate values may be obtained by use of lifting-surface theory.
Subject: AILERON
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:10:53Z | |
| date available | 2017-09-04T17:10:53Z | |
| date copyright | 01/01/1945 | |
| date issued | 1945 | |
| identifier other | YRCTUDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/134479 | |
| description abstract | INTRODUCTION One of the many aerodynamic problems for which a theoretical solution by means of lifting-line theory might be expected to be inadequate is the case of a wing in steady roll. Robert T. Jones has obtained in an unpublished analysis similar to that of reference 1 a correction to the lifting-line-theory values of the damping in roll that amounts to an B-percent reduction in the values for a wing of aspect ratio 6. Still more accurate values may be obtained by use of lifting-surface theory. | |
| language | English | |
| title | NACA-ARR-L5F23 | num |
| title | Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces | en |
| type | standard | |
| page | 56 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1945 | |
| contenttype | fulltext | |
| subject keywords | AILERON | |
| subject keywords | AILERONS | |
| subject keywords | AIRFOILS | |
| subject keywords | ANALOGY | |
| subject keywords | ASPECT | |
| subject keywords | CONTROL | |
| subject keywords | CONTROLS | |
| subject keywords | DAMPING | |
| subject keywords | DISTRIBUTION | |
| subject keywords | DOWNWASH | |
| subject keywords | ELECTROMAGNETIC | |
| subject keywords | ELLIPTICAL | |
| subject keywords | FORCES | |
| subject keywords | HINGE | |
| subject keywords | LIFT | |
| subject keywords | LIFTING | |
| subject keywords | METHOD | |
| subject keywords | MOMENTS | |
| subject keywords | RATIO | |
| subject keywords | ROLL | |
| subject keywords | STICKS | |
| subject keywords | SURFACE | |
| subject keywords | THEORIES | |
| subject keywords | WINGS |