From: Ajema S.
Category: buddhism essay
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Master thesis | ERC-AEROFLEX
Scientific context and objectives: Airfoil stall is commonly described as a sudden drop of lift when increasing the angle of attack. This phenomenon is detrimental to aircrafts and helicopters, since it strongly limits their flight envelope. Past experimental  and numerical  investigations, specifically dedicated to static stall i. The instantaneous flow slowly evolves between attached and fully separated states, resulting in large amplitude oscillations of the lift coefficient, as illustrated in Figure 1. Global stability analysis of the steady solutions has revealed the destabilization of low-frequency modes that explain the onset of the low-frequency oscillations. The objective of the thesis is to develop strategies for the control of these low-frequency oscillations.
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Since and the orbital performance of the satellite Spoutnik-1, the human activity in space has generated a growing number of space debris. In the last forty years, 16 tons of space debris have performed a terrestrial atmospheric re-entry. The total casualty area forecasting becomes a major issue for all space actors and especially for CNES, which is in charge of ensuring the strict application of the French Space Operation Law LOS by , for French satellite- and launcher-operators and for launch operations from French Guyana spaceport. The ground risk estimation is linked to a significant increase of the understanding and modelling of the physical phenomena encountered during the atmospheric entry.
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