Spiking Reinforcement Learning for Robust Robot Control Under ...

Décision du 22 mai 2006 relative à l'agrément en qualité d'hébergeur de données de santé à caractère personnel .







A ReproQQCed Copy - NASA Technical Reports Server (NTRS)
Ce volume apporte des éléments de réponse pratiques, tirés de réalisations concrètes, menées aussi bien à l'université qu'au collège, dans des médiathèques ...
Modeling of shaft precessional motions induced by unilateral and ...
This has been done with the prime purpose of determining the magnitudes of the pressure losses and the gas efflux angles from rows of turbine blades and ...
effects of operating damage of labyrinth seal - CORE
CONTENTS. 1. INTRODUCTION. 2. 1.1. Examples from the development of hydraulic machinery for electricity production in Norway 2.
An Examination of the Flow and Pressure Losses in Bfade Rows of ...
This dissertation allowed to improve an existing fixture design and to apply it from the 6?? to 9?? blade stage.
HYDRAULIC TURBINES Design, Erection and Operation By ... - NTNU
In this thesis a method to design and to analyse axial reversible turbomachinery is pre- sented. Reversible turbomachinery can act both as a compressor or ...
FIXTURE DESIGN AND CMM PROGRAM DEVELOPMENT ... - RUN
It can be used to measure movements of turbine blades, rotor-stator clearances and the degradation of TBCs. TBCs typically consist of four ...
Design and Performance Analysis of Reversible Axial ... - POLITesi
The present thesis deals with the generation of innovative design solutions for reducing aerodynamic losses in Low-Pressure. Turbines through the combined ...
Nondestructive Testing Structural Health Monitoring of Gas Turbine ...
... stator around the tips of the rotor blades. All calculated K values are considered to be the approximate machine constants of eachrotor-stator configuration.
Design Solutions for Reducing Losses in Aeronautical Low ... - FLORE
Measurements were made on and around the outlet stator row of a 1.5-stage axial compressor using thermal anemometry. Pitch-wise hot-wire probe traverses were ...
The development of a water dynamometer for turbine test applications.
Summary.--The Reynolds-number effects on the performance of a single-stage compressor have been measured over the range 0.08 × 105 to 9.0 × 105.
Unsteady boundary layer transition on axial compressor blades
the opening is a feather seal slot in a stator for a gas turbine engine, the stator having a wall extending over the slot which is thinner ...
The Effect of Reynolds Number on the Performance of a Single ...
(a) Area-averaged pressure over the R1 blade surface (b) Relationship between pressure and tip leakage flow over blade tip ... chord length of the blade ... turbine ...