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NASA-TM-4549

Effect of passive venting on static pressure distributions in cavities at subsonic and transonic speeds

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1994

Abstract: The passive venting techniques for shallow cavities that were investigated consisted of (1) porous floors, (2) slot vents at each end of solid floors, (3) slot vents at each end of porous floors, and (4) pipe vents on solid floors. For deep cavities, passive venting techniques that were investigated consisted of (1) lip vents at the outer edges of the front and rear walls of a cavity with a solid floor and (2) lip vents at the outer edges of the front and rear walls of a cavity with a porous floor. The cavity passive venting models were mounted in a flat plate model and were tested at Mach numbers from 0.20 to 0.95. The shallow cavities had lengths of 32.16 and 42.00 in. and a depth of 2.40 in., resulting in cavity length-to-depth ratios (I/h) of 13.40 and 17.50, respectively. The deep cavity had a length of 32.16 in. and a depth of 4.80 in. (I/h = 6.70). All cavities had a width of 9.60 in. Results from the test show that the porous floor and the porous floor combined with slot vents had the greatest effect on the shallow cavity pressure distributions and resulted in distributions that were representative of deeper cavities. The lip vents had little effect on the pressure distributions for the deep cavity with solid or porous floors for most of the test range of Mach number.
URI: https://yse.yabesh.ir/std/handle/yse/128643
Subject: AIRCRAFT
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    NASA-TM-4549

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:05:09Z
date available2017-09-04T17:05:09Z
date copyright01/01/1994
date issued1994
identifier otherYBNKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/128643
description abstractThe passive venting techniques for shallow cavities that were investigated consisted of (1) porous floors, (2) slot vents at each end of solid floors, (3) slot vents at each end of porous floors, and (4) pipe vents on solid floors. For deep cavities, passive venting techniques that were investigated consisted of (1) lip vents at the outer edges of the front and rear walls of a cavity with a solid floor and (2) lip vents at the outer edges of the front and rear walls of a cavity with a porous floor. The cavity passive venting models were mounted in a flat plate model and were tested at Mach numbers from 0.20 to 0.95. The shallow cavities had lengths of 32.16 and 42.00 in. and a depth of 2.40 in., resulting in cavity length-to-depth ratios (I/h) of 13.40 and 17.50, respectively. The deep cavity had a length of 32.16 in. and a depth of 4.80 in. (I/h = 6.70). All cavities had a width of 9.60 in. Results from the test show that the porous floor and the porous floor combined with slot vents had the greatest effect on the shallow cavity pressure distributions and resulted in distributions that were representative of deeper cavities. The lip vents had little effect on the pressure distributions for the deep cavity with solid or porous floors for most of the test range of Mach number.
languageEnglish
titleNASA-TM-4549num
titleEffect of passive venting on static pressure distributions in cavities at subsonic and transonic speedsen
typestandard
page180
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1994
contenttypefulltext
subject keywordsAIRCRAFT
subject keywordsCAVITIES
subject keywordsCOUNTERMEASURES
subject keywordsDISTRIBUTION
subject keywordsDRAG
subject keywordsFLAT
subject keywordsFLOW
subject keywordsMACH
subject keywordsNUMBER
subject keywordsPIPES
subject keywordsPLATES
subject keywordsPRESSURE
subject keywordsREDUCTION
subject keywordsSLOTS
subject keywordsSPEED
subject keywordsSTATIC
subject keywordsSTRUCTURES
subject keywordsSUBSONIC
subject keywordsTRANSONIC
subject keywordsTUBES
subject keywordsVENTING
subject keywordsVENTS
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