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Space Shuttle Boundary Layer Transition Flight Experiment Ground Testing OverviewIn support of the Boundary Layer Transition (BLT) Flight Experiment (FE) Project in which a manufactured protuberance tile was installed on the port wing of Space Shuttle Orbiter Discovery for STS-119, STS- 128, STS-131 and STS-133 as well as Space Shuttle Orbiter Endeavour for STS-134, a significant ground test campaign was completed. The primary goals of the test campaign were to provide ground test data to support the planning and safety certification efforts required to fly the flight experiment as well as validation for the collected flight data. These test included Arcjet testing of the tile protuberance, aerothermal testing to determine the boundary layer transition behavior and resultant surface heating and planar laser induced fluorescence (PLIF) testing in order to gain a better understanding of the flow field characteristics associated with the flight experiment. This paper provides an overview of the BLT FE Project ground testing. High-level overviews of the facilities, models, test techniques and data are presented, along with a summary of the insights gained from each test.
Document ID
20150013973
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Karen T Berger
(Langley Research Center Hampton, Virginia, United States)
Brian Paul Anderson
(Johnson Space Center Houston, Texas, United States)
Charles H Campbell
(Johnson Space Center Houston, Texas, United States)
Date Acquired
July 23, 2015
Publication Date
August 4, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-18703
Report Number: NF1676L-18703
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop (TFAWS)
Location: Cleveland, OH
Country: US
Start Date: August 4, 2014
End Date: August 8, 2014
Sponsors: Glenn Research Center
Funding Number(s)
WBS: 122711.03.07.07.06.02.80
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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