Estimation of Loads Acting on Flaps of the Su-22 Aircraft for Fatigue Tests
The paper presents the results of the calculation of forces acting on the flaps of the Su-22 aircraft during take-off and landing. Four different analytic and experimental calculation methods were used to increase the reliability of the obtained results. The results will be the basis for performance...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
Military University of Technology, Warsaw, Poland
2016-09-01
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Series: | Problemy Mechatroniki |
Subjects: | |
Online Access: | http://promechjournal.pl/gicid/01.3001.0009.2984 |