N.A.Andreeva Investigation of the possibility of control a boundary layer at the parts of fluing aircraft |
Applied hydromechanics, Vol. 1 (73) ¹ 3, (1999) |
| Here have been presented the result of the experiment-based research on a possibility to control the disperse flow round on the airfoils with on the basing signal of a thermocouple thermoanemometer - the instrument measuring low velocities of gas and liquid flows. The work offers an experimantally proven possibility to more effectively control the wing mechanization basing on the detailed data on the outer layer conditions obtained by the system of thermocouple thermoanemometer sensors. |
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| TEXT LANGUAGE: Russian |