TsAGI Science Journal
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ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604
THE INFLUENCE OF THE TRACK BEHIND THE UNDERCARRIAGE ON THE FIELD OF SPEED IN THE REGION OF A RAM AIR TURBINE
Volumen 47,
Ausgabe 6, 2016,
pp. 623-637
DOI: 10.1615/TsAGISciJ.2017019464
ABSTRAKT
The results of calculations and experimental research on the influence of the track behind the main landing gear on the velocity field in the region of a ram air turbine are presented. The numerical investigations were based on the solution to the Reynolds-averaged Navier−Stokes equations. The experiment on a model of a passenger aircraft with high-lift wings was conducted in the T-103 wind tunnel at TsAGI using an air pressure detector nozzle.
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