As part of propeller research program at Langley Research Center, dummy, nonrotating spinner was investigated over Mach number range from 0.65 to 0.95; results showed that local Mach number was less than free-stream Mach number in propeller plane but free-stream conditions were approached from about 15 to 90% of spinner length.
Flight investigation of surface pressure distribution and flow field around elliptical spinner
NASA -- Memo
1959
10 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1956
|GWLB - Gottfried Wilhelm Leibniz Bibliothek | 2017