A three-component internal strain-gauge balance for use in a cryogenic wind tunnel has been developed by National Aerospace Laboratory NLR. With this balance model tests were performed in the NASA Langley 0.3-m Transonic Cryogenic Tunnel. The results are discussed with a view to the development of strain-gauge balances for the European Transonic Wind Tunnel (ETW).
Development of a Multi-Component Internal Strain-Gauge Balance for Model Tests in a Cryogenic Wind Tunnel
1988
99 pages
Report
Keine Angabe
Englisch
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