Results of Research and Development
Fatigue crack growth tests of M(T) specimens loaded by variable amplitude, made of D16čATV and 2024-T3 alloys (LU42-2016-COC.ZK)
Publication Year: 2016
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)
Publication Year: 2016
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)
Publication Year: 2016
AUGUSTIN, P.
Life-saving equipment for unmanned air vehicles
Patent Year: 2016
POPELA, R. PEJCHAR, J. DANIEL, M. BÁBOVKA, M. NĚMČÁK, O.
Material characteristics tests of 1.6 mm thick 2524-T3 alloy sheet (LU41-2016-COC.ZK)
Publication Year: 2016
AUGUSTIN, P. ŠPLÍCHAL, J.
Modern student research and education in aircraft design
Publication Year: 2016
KATRŇÁK, T. PEJCHAR, J.
Modifications of a simple I-beam and its effects on the stress state
Publication Year: 2016
CEJPEK, J. JURAČKA, J.
Numerical Study of Benchmark Super-Critical Wing, BSCW, at Flutter Condition
Publication Year: 2016
JIRÁSEK, A. DALENBRING, M. NAVRÁTIL, J.
Overview of the basis thermal test of the heating foils for anti- icing system for aircraft leading edge.
Publication Year: 2016
KOŠTIAL, R.
Shear strength of thin web – influence of lighting openings and diagonal tension
Publication Year: 2016
HORÁK, M. PÍŠTĚK, A.
Stress Distribution Investigation at the Tapered Sandwich Endings
Publication Year: 2016
LÖFFELMANN, F.
Showed 286–300 from 980 results