TE02000032

Czech

Juračka Jaroslav, doc. Ing., Ph.D. - principal person responsible

Institute of Aerospace Engineering
- responsible department (1.1.2015 - not assigned)
Institute of Aerospace Engineering
- beneficiary (1.1.2015 - 31.12.2019)

SYMONOV, V. Bird strike simulations in MSC.Software: correlation between the experiments and simulations. In 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021. 32nd Congress of the International Council of the Aeronautical Sciences, Shanghai, China: ICAS, 2021. p. 1-11. ISBN: 9783932182914.
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SYMONOV, V.; JURAČKA, J. Bird strike simulations in MSC.Software: correlation between the experiments and simulations. 32nd Congress of the International Council of the Aeronautical Sciences: 2021.
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URÍK, T. Výzkum vlivu technologie zhotovení nýtových spojů II (LU24-2015-COC.SD). 2015.
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AUGUSTIN, P.; ŠPLÍCHAL, J. Únavové zkoušky lícovaných šroubů ONL 3120 průměru 6 mm z různých materiálů (LU31-2019-COC.ZK). 2019.
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AUGUSTIN, P. Únavové zkoušky lícovaných šroubů ONL 3120 průměru 12 mm z různých materiálů (LU32-2019-COC.ZK). 2019.
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AUGUSTIN, P. Metodika únavových zkoušek lícovaných šroubů ONL 3120 z různých materiálů (LU26-2018-COC.ZK). 2018.
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AUGUSTIN, P. Specification of recommended materials and semi-finished products for DT structures (LU58-2017-COC.ZK). 2017.
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AUGUSTIN, P.; ŠPLÍCHAL, J. Material characteristics tests of D16čT aluminum alloy (LU48-2017-COC.ZK). 2017.
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AUGUSTIN, P. Fatigue crack growth tests of AISI 4340 AQ steel (LU24-2017-COC.ZK). 2017.
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AUGUSTIN, P. Fatigue test of the lugs made of AISI 4340 steel (LU27-2018-COC.ZK). 2018.
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AUGUSTIN, P. Fatigue test of welded engine mount rod made of AISI 4130 steel (LU16-2017-COC.ZK). 2017.
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AUGUSTIN, P. Fatigue test of flap hinge made of castaluminum alloy (LU7-2017-COC.ZK). 2017.
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AUGUSTIN, P. Fatigue crack growth tests of M(T) specimens loaded by variable amplitude, made of D16čATV and 2024-T3 alloys (LU42-2016-COC.ZK). 2016.
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AUGUSTIN, P. Fatigue crack growth tests of M(T) specimens loaded by variable amplitude, made of 7475-T7351 and 2124-T851 alloys (LU15-2016-COC.ZK). 2016.
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AUGUSTIN, P. Fatigue crack growth tests of M(T) specimens loaded by variable amplitude, made of 7475-T7351, 2124-T851 and 7050-T7451 alloys (LU9-2016-COC.ZK). 2016.
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AUGUSTIN, P. Fatigue crack growth tests of M(T) specimens loaded by variable amplitude, made of AISI 4340 AQ steel (LU10-2017-COC.ZK). 2017.
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AUGUSTIN, P. Fatigue crack growth test of M(T) specimens, made of 7475-T7351 and 2124-T851 alloys, for verification of mean stress effect (LU4-2017-COC.ZK). 2017.
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JURAČKA, J. Návrh metod pro analýzy postupného poškozování. Brno: LU FSI VUT v Brně, 2017. s. 1-47.
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AUGUSTIN, P. Fatigue test of main landing gear actuator pin made of AISI 4340 steel (LU28-2019-COC.ZK). 2019.
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AUGUSTIN, P.; ŠPLÍCHAL, J. Material characteristics tests of 1.6 mm thick 2524-T3 alloy sheet (LU41-2016-COC.ZK). 2016.
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Responsibility: Juračka Jaroslav, doc. Ing., Ph.D.