This paper is the first part of a 2D description of a single crystal thin plate growth by micro-pulling–down (μ-PD) method. This part concerns the following aspects: the free surface equation and the pressure difference...
The main objective of this paper is to describe a code for calculating an equivalent system of concentrate loads for a FEM analysis. The tables from the Aerodynamic Department contain pressure field for a whole bearing s...
The paper presents some methods of on-ground and in-flight calibration for strain gauges, intended to the development of complex programs which analyze the endurance phenomena for aerospace structures, with direct applic...
Fault tree analysis is a deductive approach for resolving an undesired event into its causes, identifying the causes of a failure and providing a framework for a qualitative and quantitative evaluation of the top event....
The preparation of atmospheric Earth reentry vehicles requires the estimation of heat and mechanical loads along the trajectory, as well as the impact point. A dedicated tool for axial symmetric capsules is prepared for...
EP ID EP119328
DOI 10.13111/2066-8201.2011.3.S9
Views 73
Downloads 0
How To Cite
Ion STROESCU (2011). “Noui Perspective in Aerodinamica Avionului” - 1925
(selected pages). INCAS BULLETIN, 3(0),
79-88. https://europub.co.uk/articles/-A-119328
Sign In Europub
For faster login or register use your social account.
A 2D description of the single crystal thin plate growth from the melt by micro - pulling - down method. Part 1
This paper is the first part of a 2D description of a single crystal thin plate growth by micro-pulling–down (μ-PD) method. This part concerns the following aspects: the free surface equation and the pressure difference...
[b]ALOAD - a code to determine the concentrated forces equivalent with a distributed pressure field for a FEM analysis[/b]
The main objective of this paper is to describe a code for calculating an equivalent system of concentrate loads for a FEM analysis. The tables from the Aerodynamic Department contain pressure field for a whole bearing s...
Comprehensive study of endurance for IAR-99 Hawk
The paper presents some methods of on-ground and in-flight calibration for strain gauges, intended to the development of complex programs which analyze the endurance phenomena for aerospace structures, with direct applic...
Boolean Algebra Application in Analysis of Flight Accidents
Fault tree analysis is a deductive approach for resolving an undesired event into its causes, identifying the causes of a failure and providing a framework for a qualitative and quantitative evaluation of the top event....
Earth Reentry Tool for Preliminary Mission Analysis
The preparation of atmospheric Earth reentry vehicles requires the estimation of heat and mechanical loads along the trajectory, as well as the impact point. A dedicated tool for axial symmetric capsules is prepared for...