NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
The Design and Use of Calorimeters For Characterization of High-Enthalpy Flows in Arc-Heated Test FacilitiesHigh-enthalpy, arc-heated flows used for aerothermal testing present a challenging environment for flow characterization. This paper describes the design and use of cooled dwell probes used for heat-transfer and pressure characterization of the NASA and United States Department of Defense (DoD) arc facilities located at Moffett Field, CA, and Arnold Air Force Base, TN. Dwell calorimeters designed, fabricated, and tested by Thermal Technologies, Inc. (TTI) in the NASA IHF and the USAF H1 and H2 arc test facilities provide heat flux and pressure data with excellent repeatability. These calorimeters use standard Gardon calorimeter gages and pressure ports with unique cooling systems enabling them to withstand the severe arc-heated environments for durations sufficient for acquisition of steady-state data. The TTI probes have proven very robust in the extreme aerothermal environments of these facilities. This paper provides an overview of calorimeter instruments typically used in arc facilities, discusses design features of the TTI dwell probes, presents selected data acquired by the TTI calorimeters, and provides comparisons with data acquired from using measurement techniques.
Document ID
20260005828
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
D Mark Smith
(Arnold Engineering Development Center Arnold AFS, TN, United States)
Henry Moody
(Thermal Technologies (United States) Cambridge, United States)
Chris Wanstall
(Southern Research Institute Durham, United States)
Imelda Terrazas-Salinas
(Ames Research Center Mountain View, United States)
Date Acquired
June 29, 2026
Publication Date
September 29, 2002
Publication Information
Publication: AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference
Publisher: American Institute of Aeronautics and Astronautics
e-ISBN: 9781624101236
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
AIAA-2002-5236
Meeting Information
Meeting: 11th AIAA/AAAF International Conference Space Plane and Hypersonic Systems and Technologies
Location: Orleans
Country: FR
Start Date: September 29, 2002
End Date: October 4, 2002
Sponsors: American Institute of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
No Preview Available