Документ взят из кэша поисковой машины. Адрес оригинального документа : http://termogaz.imec.msu.ru/our_oppoturn/our_oppoturn_e.htm Дата изменения: Mon Mar 30 10:11:27 2009 Дата индексирования: Mon Oct 1 19:36:27 2012 Кодировка:

Our abilities
	Simultaneous measurement of local heat transfer and pressure drag coefficients on a smooth surface and a surface with complex relief (dimples, projections, grooves etc.), flown over by subsonic air stream, with velocity range from 5 m/s to 120 m/s.
	Simultaneous measurement of local coefficients of heat transfer and pressure drag on smooth surface and surface with complex relief (dimples, projections, grooves etc.), flown by supersonic air stream, with velocity range corresponding with Much Number: 1,2; 1,3; 1,75; 2,0; 2,5; 2,8.
	Measurement of local coefficients of heat transfer models and surfaces flown over by supersonic air stream by transient method.
	Measurement of thermal protection efficiency with the use of porous cooling and gas curtains.
	Visualization of supersonic gas flows by means of IAB-451.
	Acquisition of temperature field on the surfaces, flown over by supersonic air stream, with the use of infrared image camera ThermaCAM SC 3000 and infrared windows (polycrystalline ZnSe).
	Acquisition, processing, visualization and storage of information about research parameters, with the use of high-performance ADC National Instruments, software LabVIEW 7.1, modern computer equipment.