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TPSAS-NF1676L-32584-DNDCryogenic, 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 and execution, and the discussion of other in-depth technical topics. This particular presentation supports a section of model preparation, tunnel operations, and model access procedures that are unique to cryogenic wind-tunnel testing.
Document ID
20200005420
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Scott Goodliff
(Jacobs (United States) Dallas, Texas, United States)
Date Acquired
May 11, 2020
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NF1676L-32584
Report Number: NF1676L-32584
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
CONTRACT_GRANT: NNL13AA14C
Distribution Limits
Public
Copyright
Public Use Permitted.
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