NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
BOLT II Roughness-Side Flight ResultsAn initial review of the roughness data from the BOLT II flight is provided. The BOLT II roughness experiment was designed to investigate discrete trips in flight based on the diamond configuration, which has been shown to be an efficient vortex generator and boundary layer trip from extensive ground-based testing. There were three trip locations chosen for the flight test and their size (height and width) were tailored to the local boundary layer thickness, but all three were expected to trip at the same time or flight condition. Details about the flight vehicle design, instrumentation, and best estimated trajectory are discussed. The present paper is limited to only a review and analysis of the thermocouple data. Boundary layer transition onset times are derived from the thermocouple analysis, thus allowing an initial assessment of the performance of these discrete trips. Since the three trips were sized to trip the boundary layer at the same time, based on a previous wind tunnel study, the present analysis indicates that they performed as expected.
Document ID
20220018015
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Scott A. Berry
(Langley Research Center Hampton, Virginia, United States)
Brad Wheaton
(Johns Hopkins University Applied Physics Laboratory North Laurel, Maryland, United States)
Date Acquired
November 29, 2022
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AIAA SciTech23
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 725017.02.07.03.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
Hypersonic
Boundary Layer Transition
Roughness
No Preview Available