SIMULAND - A CODE TO ANALYZE DYNAMIC EFFECTS DURING LANDING
Journal Title: INCAS BULLETIN - Year 2010, Vol 2, Issue 1
Abstract
The landing gear of an aircraft is part of the aircraft structure. It is the most critical part of the flight mission and also the component that will likely cause the most problems in the aircraft design. The landing gear design combines the best in mechanical, structural and hydraulic design. The designed landing gear should be able to meet the specifications and requirements imposed by the CS23. SIMULAND-01 is a program intended to analyze a reduced model (4-30 DoF) of the aircraft under transient dynamic loads during the landing phase (touchdown).
Authors and Affiliations
Daniela BARAN, Marcel STERE, Nicolae APOSTOLESCU
Keywords
Related Articles
- EP ID EP134578
- DOI 10.13111/2066-8201.2010.2.1.1
- Views 89
- Downloads 0
Parameters monitoring and control for flueric actuators testing system
A wide range of air supply parameters is needed for the flueric actuators testing in order to find their optimum working regime. A system for conditioning these parameters, namely pressure, temperature, mass and volume f...
Turboprop Engine Nacelle Optimization for Flight Increased Safety and Pollution Reduction
Commuter airplanes defined in CS-23 as being propeller driven, twin-engine, nineteen seats and maximum certified take-off weight of 8618 Kg had lately a special development due to advantages of turboprop engine compared...
Magnetic field nanosensor based on Mn impurities
Nanosensors based on graphene nanoribbon, studied in the present work, could provide a special interest in (aero) space applications. More specifically, the paper proposes the construction of a nanosensor based on Mn (Ma...
ELIE CARAFOLI AT THE ROMANIAN ACADEMY
A new solid particle erosion model for oriented fiber composite materials
The work describes a new model of erosion estimation equation which factors in both the impingement angle α and the fiber orientation angle β. Two examples of particular erosion equations are presented, for carbon fiber...