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Fractographic reconstitution of fatigue crack growth in integrally stiffened panels
-by-flight spectrum loading and testing the effectiveness of various fractographic kinds of cyclic loading were used: constant amplitude loading (CAL), flight-by-flight type spectrum<...
JL - Únava materiálu a lomová mechanika
- 2010 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Fractographic Analysis of Integrally Stiffened Panels for Airplane Wing
panels during the fatigue tests under flight-by-flight spectrum loading. The panels were tested by three kinds of cyclic loading, i.e., constant amplitude loading and flight-by-fligh...
JL - Únava materiálu a lomová mechanika
- 2010 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Fractographic Analysis of Fatigued Integral Panels of Aircraft Wing
during the fatigue tests under flight-by-flight spectrum loading. These panels, based onthe redistribution of individual flights in the original loading sequence to the influence of the loadi...
JL - Únava materiálu a lomová mechanika
- 2009 •
- D
Rok uplatnění
D - Stať ve sborníku
Comparison of heart rate response to + and ? Gz load changes at safe and low altitude level during real flight
Low level flight systems with possibilities to follow terrain expose pilots of agile combat aircraft to a new flight load. A new quality of the flight load of the pilot?s physiological response to the ...
KA - Vojenství
- 2003 •
- Jx
Rok uplatnění
Jx - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)
Testing method of plus and minus Gz tolerance at Czech Air Force pilots
Low level flight systems with possibilities to follow terrain expose pilots of agile combat aircraft to a new flight load. A new quality of the flight load of the pilot?s physiological response to the ...
KA - Vojenství
- 2004 •
- D
Rok uplatnění
D - Stať ve sborníku
Comparison of Cardiovascular Response to + and ? Gz Load Changes at safe and low Altitude Level during real Flight.
Low level flight systems with possibilities to follow terrain expose pilots of agile combat aircraft to a new flight load. A new quality of the flight load to this load type. A method with an eval...
FP - Ostatní lékařské obory
- 2003 •
- D
Rok uplatnění
D - Stať ve sborníku
Report LU51-2020-TAG.AD-version IR - Aerostatic documentation for flight loading calculation - TAG 21m
This report contains aerostatic documentation for flight loading calculation of TAG wing in 21 m variant.
Aerospace engineering
- 2020 •
- O
Rok uplatnění
O - Ostatní výsledky
Flight by Flight Fatigue Test of Aircraft Structure
of an aircraft structure is a random application of loads on a flight by flight basis. This paper deals with the development of such load sequence which simulates a load historyas it can occur in service....
JL - Únava materiálu a lomová mechanika
- 2003 •
- D
Rok uplatnění
D - Stať ve sborníku
Flight by Flight Fatigue Test of Aircraft Structure
of an aircraft structure is a random application of loads on a flight by flight basis. This paper deals with the development of such load sequence which simulates a load historyas it can occur in service....
JL - Únava materiálu a lomová mechanika
- 2003 •
- D
Rok uplatnění
D - Stať ve sborníku
Measuring of a Nose Landing Gear Loads
The publication describes the in flight measurement of the load on the nose landing gear of the aircraft.
JU - Aeronautika, aerodynamika, letadla
- 2015 •
- Vsouhrn
Rok uplatnění
Vsouhrn - Souhrnná výzkumná zpráva
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