NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
NASA's Turbulent Heat Flux (THX) Experiments This presentation will give an overview of the NASA Turbulent Heat Flux (THX) experiments. This work was conducted at NASA Glenn Research Center (GRC) to collect measurements of velocities and temperatures for computational fluid dynamics (CFD) validation of heated flows, with a focus on propulsion system components. The experiments were conducted in 5 phases; four of which were conducted in the GRC Aeroacoustic Propulsion Laboratory (AAPL) using the Small Hot Jet Flow Rig (SHJAR). In addition, computational studies were also conducted for the experimental configurations, in order to provide a baseline of expected CFD results and to make an assessment of the capability of various CFD approached for calculating flows where the turbulent transport of heat was important. Two of the collected sets of data were also used for American Institute of Aeronautics and Astronautics (AIAA) Propulsion Aerodynamic Workshops (PAWs). The data set from the 5th phases, collected for heated supersonic jets, was also used to construct new validation cases for the NASA Turbulence Model Resource (TMR).
Document ID
20250004781
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Nick Georgiadis
(Glenn Research Center Cleveland, United States)
Mark Wernet
(Glenn Research Center Cleveland, United States)
Date Acquired
May 8, 2025
Subject Category
Aircraft Propulsion and Power
Meeting Information
Meeting: TTT-RCA High Fidelity CFD Workshop
Location: Suffolk, VA
Country: US
Start Date: May 20, 2025
End Date: May 22, 2025
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 109492.02.03.05.01.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
supersonic jet
turbulence
convergent-divergent nozzle
LES
RANS
No Preview Available