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NASA MEMO 6-5-59 REV A

Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of the Static and Dynamic Stability Derivatives of an Airplane Model with an Unswept Wing and a High Horizontal Tail

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1959

Abstract: Results are presented of a wind-tunnel investigation to evaluate the static and dynamic stability derivatives of a model with a low-aspect-ratio unswept wing and a high horizontal tail. In addition to results for the complete model, results were also obtained of the body alone, body and wing, and body and tail. Data were obtained in the Mach number range from 0.65 to 2.2, at a Reynolds number of 2 million based on the wing mean aerodynamic chord. The angle-off attack range for most of the data was -11.5º to 180º. A limited amount of data was obtained with fixed transition.
URI: https://yse.yabesh.ir/std/handle/yse/21167
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    NASA MEMO 6-5-59 REV A

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:21:10Z
date available2017-09-04T15:21:10Z
date copyright01/01/1959
date issued1959
identifier otherMYMKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/21167
description abstractResults are presented of a wind-tunnel investigation to evaluate the static and dynamic stability derivatives of a model with a low-aspect-ratio unswept wing and a high horizontal tail. In addition to results for the complete model, results were also obtained of the body alone, body and wing, and body and tail. Data were obtained in the Mach number range from 0.65 to 2.2, at a Reynolds number of 2 million based on the wing mean aerodynamic chord. The angle-off attack range for most of the data was -11.5º to 180º. A limited amount of data was obtained with fixed transition.
languageEnglish
titleNASA MEMO 6-5-59 REV Anum
titleWind-Tunnel Investigation at Subsonic and Supersonic Speeds of the Static and Dynamic Stability Derivatives of an Airplane Model with an Unswept Wing and a High Horizontal Tailen
typestandard
page80
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1959
contenttypefulltext
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