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NASA-LLIS-0562

Lessons Learned – Testing With Removable Shrouds in the LaRC 8-Foot High Temperature Tunnel

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1997

Abstract: Description of Driving Event:
A model under test in the tunnel required the use of a removable shroud to insulate a sensor from heating while the model was being injected into the tunnel flow. Once the model was in the tunnel flow and was ready to collect data, the shroud was released from the model and ejected from the diffuser of the tunnel. The first test used a metal shroud that had been designed with air dams to ensure that it was not aerodynamic. The metal shroud was of sufficient mass and was ejected from the tunnel at sufficient velocity to cause the shroud to travel a long distance placing personnel in its potential path at unacceptable risk. A "catcher screen" was install but was not successful in capturing the metal shroud. The metal shroud was replaced with a wooden shroud. The wooden shroud provided the needed heat protection for the sensor and upon release, tumbled, contacted the diffuser walls of the tunnel and disintegrated. The pieces of the wooden shroud either came to rest before reaching the catcher screen or were captured by the catcher screen
URI: https://yse.yabesh.ir/std/handle/yse/32018
Subject: Test & Verification
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NASA-LLIS-0562

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:30:37Z
date available2017-09-04T15:30:37Z
date copyright09/04/1997
date issued1997
identifier otherOBCEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/32018
description abstractDescription of Driving Event:
A model under test in the tunnel required the use of a removable shroud to insulate a sensor from heating while the model was being injected into the tunnel flow. Once the model was in the tunnel flow and was ready to collect data, the shroud was released from the model and ejected from the diffuser of the tunnel. The first test used a metal shroud that had been designed with air dams to ensure that it was not aerodynamic. The metal shroud was of sufficient mass and was ejected from the tunnel at sufficient velocity to cause the shroud to travel a long distance placing personnel in its potential path at unacceptable risk. A "catcher screen" was install but was not successful in capturing the metal shroud. The metal shroud was replaced with a wooden shroud. The wooden shroud provided the needed heat protection for the sensor and upon release, tumbled, contacted the diffuser walls of the tunnel and disintegrated. The pieces of the wooden shroud either came to rest before reaching the catcher screen or were captured by the catcher screen
languageEnglish
titleNASA-LLIS-0562num
titleLessons Learned – Testing With Removable Shrouds in the LaRC 8-Foot High Temperature Tunnelen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1997
contenttypefulltext
subject keywordsTest & Verification
subject keywordsTest Facility
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DSpace software copyright © 2017-2020  DuraSpace
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