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NASA-TP-1157
Ground distance covered during airborne horizontal deceleration of an airplane
Year: 1978
Abstract: The distance an airplane floats with respect to the ground during deceleration at constant altitude is analyzed taking into account the effects of a constant wind. By use of suitable nondimensionalizing parameters, data applicable to all airplanes are presented by means of a single family of curves.
Subject: AIRCRAFT LANDING
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:39:48Z | |
| date available | 2017-09-04T16:39:48Z | |
| date copyright | 01/01/1978 | |
| date issued | 1978 | |
| identifier other | VMBBFEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/103486 | |
| description abstract | The distance an airplane floats with respect to the ground during deceleration at constant altitude is analyzed taking into account the effects of a constant wind. By use of suitable nondimensionalizing parameters, data applicable to all airplanes are presented by means of a single family of curves. | |
| language | English | |
| title | NASA-TP-1157 | num |
| title | Ground distance covered during airborne horizontal deceleration of an airplane | en |
| type | standard | |
| page | 14 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1978 | |
| contenttype | fulltext | |
| subject keywords | AIRCRAFT LANDING | |
| subject keywords | DECELERATION | |
| subject keywords | DRAG REDUCTION | |
| subject keywords | FLOATING | |
| subject keywords | GENERAL AVIATION AIRCRAFT | |
| subject keywords | GROUND EFFECT (AERODYNAMICS) | |
| subject keywords | GROUND WIND | |
| subject keywords | LANDING LOADS | |
| subject keywords | LANDING SPEED | |
| subject keywords | LIFT |