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BOLT II Forebody Surface Measurement AnalysisSurface impression molds of the nosetip/forebody interface, discrete tripping elements, and other surface imperfections were formed on the BOLT II flight vehicle prior to its launch in March 2022. The silicon-rubber molds cast on the interface between the nickel nosetip and the stainless steel forebody were measured using a 3D optical measurement system and a stylus profilometer and were evaluated for step direction and height. The step around the nosetip/forebody interface was found to vary in both magnitude and direction, but values were generally modest with most samples below 60 μm across the span and only two samples, both cast in the gutter, with step values larger than 100 μm. Impressions of the secondary-side tripping elements were strictly scanned with the optical device and similar methods were used to calculate trip height as step height. The measured centerline trip height was 2623 ±12 μm, while the leading-edge, quadrant 2 and 3, trip heights were 897 ±5 μm and 891 ±18 μm, respectively. Surface imperfections on the nose and forebody were also evaluated. Surface roughness values and spectra were estimated, and profiles were extracted across the imperfections to quantify the magnitude of those features.
Document ID
20230000169
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Andrew N Leidy
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
January 6, 2023
Publication Date
January 1, 2023
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
NASA/TM-20230000169
Funding Number(s)
WBS: 725017.02.07.03.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Trip height
Step height
Profilometry
Surface roughness
Surface impression molds
BOLT II
Boundary layer transition
Turbulence
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