NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Material Response Modeling of MMOD CavitiesAn arc-jet test campaign is used as a baseline to computationally model the flow and material response of cavities. A parametric study is designed around the baseline to study geometric effects on parameters of interest. The US3D flow solver is used to simulate the arc-jet flow in the Aerodynamic Heating Facility (AHF) at NASA Ames and generate the heating environment over material samples with cavities. The Icarus material response code is then used to simulate the multi-dimensional heating under the above conditions of samples of FiberForm with cavities.
Document ID
20210025627
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Olivia M Schroeder
(University of Minnesota Minneapolis, Minnesota, United States)
Prakash Shrestha
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Grant Palmer
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Eric Stern
(Ames Research Center Mountain View, California, United States)
Graham V. Candler
(University of Minnesota Minneapolis, Minnesota, United States)
Date Acquired
December 7, 2021
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AIAA SciTech Forum
Location: San Diego, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80NSSC18K1150
CONTRACT_GRANT: N00014-20-1-2682
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
EDL
Aerothermodynamics
TPS
CFD
No Preview Available