The transonic wind tunnel Braunschweig is a pressurized blowdown wind tunnel. The test section for two-dimensional airfoil testing has an area of 0.34 x 0.60 m. Mach number range is from 0.3 to 0.95 and Reynolds number range from 2,900,000 to 12 million at Mach 0.7, based on an airfoil chord length of 150 mm. Information required for the preliminary planning of test programs and for preliminary layout of models used in such programs is given.
Transonic Wind Tunnel (TWB) at Dfvlr in Braunschweig (Federal Republic of Germany)
1988
45 pages
Report
No indication
English
Transonic Wing Dfvlr-F4 as European Test Model
NTIS | 1980
|Transonic wing DFVLR-F4 as European test model
NTRS | 1980
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