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Data Reduction and CorrectionsCryogenic high-Reynolds number testing has been in use for approximately 40 years. This reliable testing capability is used to more closely predict full-scale flight aerodynamics for improved accuracy in estimates of aircraft performance, stability, and loads. A technical course has been created to educate industry, institutional, and research professionals in the overview of cryogenic high-Reynolds number testing and its impact, the availability and accessibility of cryogenic testing and considerations in test planning an execution, and the discussion of other in-depth technical topics. This particular presentation supports a section relating to special data reduction and correction methods as they relate to high-Reynolds number cryogenic wind-tunnel testing.
Document ID
20200003414
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Scott Goodliff
(Jacobs (United States) Dallas, Texas, United States)
Date Acquired
May 8, 2020
Publication Date
May 14, 2019
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-33031
Report Number: NF1676L-33031
Meeting Information
Meeting: AVT-328 Impact and Advanced Implementation of Cryogenics in Aerodynamic Testing
Location: Cologne
Country: DE
Start Date: May 14, 2019
End Date: May 16, 2019
Sponsors: North Atlantic Treaty Organization
Funding Number(s)
WBS: 432938.11.01.07.43.40.27
Distribution Limits
Public
Copyright
Public Use Permitted.
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