NASA NTRS ยท 20200003414
TPSAS-NF1676L-33031-DND
Abstract
Cryogenic 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.
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Scott Goodliff. 2019-05-14. TPSAS-NF1676L-33031-DND. https://ntrs.nasa.gov/citations/20200003414
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