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NACA-TN-3393

An experimental investigation of the base pressure characteristics of nonlifting bodies of revolution at Mach numbers from 2.73 to 4.98

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1955

Abstract: An investigation was undertaken in the Ames 10- by 14-inch super-sonic wing tunnel to determine some of the base pressure characteristics of related bodies of revolution at zero angle of attack. The basic body shape used in this investigation was a 10-caliber tangent ogive nose section combine with a cylindrical afterbody. Other related shapes tested differed in that they had either a blunt-nosed profile or a boat-tailed afterbody. Model finess ratios were varied from 3.12 to 10 by changing afterbody length. Tests were conducted at free-stream Mach numbers from 2.73 to 4.98 over a Reynolds number range, based on body length, from 0.6 x 108 to 8.8 x 106.
URI: https://yse.yabesh.ir/std/handle/yse/111286
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    NACA-TN-3393

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:47:54Z
date available2017-09-04T16:47:54Z
date copyright01/01/1955
date issued1955
identifier otherWGOUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/111286
description abstractAn investigation was undertaken in the Ames 10- by 14-inch super-sonic wing tunnel to determine some of the base pressure characteristics of related bodies of revolution at zero angle of attack. The basic body shape used in this investigation was a 10-caliber tangent ogive nose section combine with a cylindrical afterbody. Other related shapes tested differed in that they had either a blunt-nosed profile or a boat-tailed afterbody. Model finess ratios were varied from 3.12 to 10 by changing afterbody length. Tests were conducted at free-stream Mach numbers from 2.73 to 4.98 over a Reynolds number range, based on body length, from 0.6 x 108 to 8.8 x 106.
languageEnglish
titleNACA-TN-3393num
titleAn experimental investigation of the base pressure characteristics of nonlifting bodies of revolution at Mach numbers from 2.73 to 4.98en
typestandard
page46
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1955
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
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