NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Evaluation of CFD as a Surrogate for Mach 2.4 to 4.6 Wind-Tunnel Testing - Project OverviewThis slide package describes the project currently evaluating the ability of CFD to take on the role of the Langley Unitary Plan Wind Tunnel should the wind tunnel be demolished as currently planned in 2022.
Document ID
20210017922
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Jim Ross
(Ames Research Center Mountain View, California, United States)
Matthew Rhode
(Langley Research Center Hampton, Virginia, United States)
Bryan Falman
(Jacobs (United States) Dallas, Texas, United States)
Karl Edquist
(Langley Research Center Hampton, Virginia, United States)
Mark Schoenenberger
(Langley Research Center Hampton, Virginia, United States)
Gregory Brauckmann
(Langley Research Center Hampton, Virginia, United States)
Bil Kleb
(Langley Research Center Hampton, Virginia, United States)
Thomas West
(Langley Research Center Hampton, Virginia, United States)
Stephen Alter
(Langley Research Center Hampton, Virginia, United States)
David Witte
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
June 24, 2021
Subject Category
Aerodynamics
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AIAA Aviation Forum
Location: Virtual
Country: US
Start Date: August 2, 2021
End Date: August 6, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 951888.06.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
wind tunnel testing
Computational Fluid Dynamics
No Preview Available