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Hiroshi Yamashita

Researcher at German Aerospace Center

Publications -  20
Citations -  252

Hiroshi Yamashita is an academic researcher from German Aerospace Center. The author has contributed to research in topics: Air traffic control & Climate change. The author has an hindex of 7, co-authored 18 publications receiving 165 citations.

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Mitigating the Climate Impact from Aviation: Achievements and Results of the DLR WeCare Project

TL;DR: The WeCare project (Utilizing Weather information for Climate efficient and eco-efficient future aviation) as mentioned in this paper aimed at finding solutions for reducing the climate impact of aviation based on an improved understanding of the atmospheric impact from aviation by making use of measurements and modeling approaches.
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A Concept for Multi-Criteria Environmental Assessment of Aircraft Trajectories

TL;DR: In this paper, the authors present a mathematical framework for environmental assessment and optimisation of aircraft trajectories based on environmental change functions (ECFs), which represent environmental impact due to changes in air quality, noise and climate impact.
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Impact on flight trajectory characteristics when avoiding the formation of persistent contrails for transatlantic flights

TL;DR: In this paper, the impacts on flight trajectories, such as lateral and vertical changes, when avoiding the formation of persistent contrails for transatlantic flights were studied, and the trade-off between the flight time and contrail distance showed a large daily variability, meaning for the same increase in flight time, the reduction in contrail distances varies from 20 to 80 depending on the daily meteorological situation.
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Newly developed aircraft routing options for air traffic simulation in the chemistry–climate model EMAC 2.53: AirTraf 2.0

TL;DR: The results clearly show that AirTraf 2.0 can find the different families of optimum flight trajectories (three-dimensional) for specific routing options; those trajectories minimize the corresponding objective functions successfully.
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Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing

TL;DR: In this article, the authors describe the start/unstart characteristics of a finite and rectangular supersonic biplane wing with an aspect ratio of 0.75 and 2.5.