FORMATION ENERGETIC ACTIVITY OF HIGH-FREQUENCY ACOUSTIC FIELDS
Journal: International Scientific Journal "Internauka" (Vol.2, No. 11)Publication Date: 2016-11-30
Authors : Shybetskyy V.; Fesenko S.;
Page : 108-110
Keywords : N-wave; hypersonic aircraft; caustic zone; wave coincidence; float gyroscope;
Abstract
The computational model of additional errors, which occur from interaction of intense shock N-wave with inertial positioning devices of hypersonic aircraft was built. Angles of coincidence for the industrial design of the angular velocity sensor were fitted. A comparative analysis of the experimental data for seminatural conditions for the two cases (gyroscope ON, gyroscope OFF) was made. Conclusions about the possibility of use of the results were made.
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