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High reynolds number tools and techniques for civil aircraft design - an overview of the HiReTT programme 民用飞机设计的高雷诺数工具和技术——HiReTT计划综述
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90069-3
Stephen Rolston (Engineering Team Leader)

The collaborative research project HiReTT, coordinated by Airbus UK, is focused on understanding the effects of scale on aircraft drag. The project was launched in January 2000 as part of the European Fifth Framework Programme. In this paper an overview of the HiReTT project objectives and work plan is given to together with progress achieved in the first year of the project. The improvement in analysis tools and test techniques delivered by this programme will enable an accurate prediction of aircraft performance to be made with the aircraft design process that can be validated ahead of first flight.

由英国空中客车公司协调的合作研究项目HiReTT专注于了解规模对飞机阻力的影响。该项目于2000年1月启动，是欧洲第五框架方案的一部分。本文概述了HiReTT项目的目标和工作计划，以及项目第一年取得的进展。该方案提供的分析工具和测试技术的改进将使飞机设计过程能够准确预测飞机性能，并在首次飞行前进行验证。
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引用次数: 10
Braking systems — Towards modular architectures and smart modules — the SAMBA project 制动系统——迈向模块化架构和智能模块——SAMBA项目
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90091-7
Laure Girault

The use of smart actuators, in a modular braking system architecture, offers the possibility of simplifying central braking control and of developing versatile standard components applicable to braking systems in different families of aircraft. The SAMBA (Smart Actuator and Modular Braking Application) project has investigated these possibilities together with techniques for control of brake torque instead of brake pressure.

在模块化制动系统架构中使用智能致动器，提供了简化中央制动控制和开发适用于不同系列飞机制动系统的通用标准部件的可能性。SAMBA（智能执行器和模块化制动应用）项目研究了这些可能性，以及控制制动扭矩而不是制动压力的技术。
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引用次数: 2
Viscous flow simulation tools - validity, robustness and efficiency of modern flow solvers: AVTAC 粘性流模拟工具-现代流求解器的有效性、稳健性和效率：AVTAC
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90070-X
Eberhard Elsholz, Alan R.B. Gould

The AVTAC project had been a large scale industrial validation and code improvement effort, dealing with fairly complex configurations at a two-equation level of turbulence modelling.

AVTAC项目是一项大规模的工业验证和代码改进工作，在湍流建模的两方程水平上处理相当复杂的配置。
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引用次数: 0
Flight safety, aircraft vortex wake and airport operation capacity 飞行安全、飞机涡流尾流和机场运营能力
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90096-6
Victor V. Vyshinsky (Deputy Head)

One of the major problems that challenge today's aeronautics is the problem of improving flight safety. A zone of increased hazard is the aerospace in the vicinity of an airport. Here, one of aircraft accidents' causes is wake turbulence generated by aircraft. The encountering of an aircraft on take-off or landing with the vortex wake of a preceding aircraft can lead to an accident especially dangerous near the ground.

当今航空面临的主要挑战之一是提高飞行安全性的问题。危险增加的区域是机场附近的航空航天。在这里，飞机事故的原因之一是飞机产生的尾流湍流。飞机在起飞或降落时遇到前一架飞机的涡流尾流，可能会导致在地面附近发生特别危险的事故。
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引用次数: 6
Efficient design and certification of advanced composite structures 先进复合结构的高效设计和认证
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90074-7
Tomas Ireman, L. Asp
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引用次数: 5
The challenge of reducing both airframe weight and manufacturing cost 降低机身重量和制造成本的挑战
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90072-3
J. Hinrichsen, C. Bautista
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引用次数: 66
HeliSafe® — EU research into occupant safety in helicopter crashes HeliSafe®-欧盟对直升机事故中乘员安全的研究
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90101-7
U. Hessmer
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引用次数: 4
Industry's perspective of European aeronautics research and technology 工业界对欧洲航空研究和技术的看法
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90043-7
Rainer Hertrich
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引用次数: 1
HITS - High Insulation Thermal Barrier Coating systems HITS -高绝缘热障涂层系统
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90086-3
B. Saint-Ramond
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引用次数: 13
The ‘MOB’ project: towards methods to support e-design across Europe “MOB”项目:寻求支持整个欧洲电子设计的方法
Air & Space Europe
Pub Date : 2001-05-01 DOI: 10.1016/S1290-0958(01)90061-9
Alan Morris

The development of the MDO approach presented in this paper is based on extensive programmes of research undertaken in the aerospace sector. Some of this work has resulted from in-house development of systems to support the creation of actual production aircraft of which references (1) and (2) are typical examples. Other studies have focused on the development of methods to support the application of MDO using a variety of optimisation approaches mainly in the conceptual or early preliminary design phases (2–6) and in the opportunities provided by large scale computing (7). The most detailed application for a realistic aircraft component was undertaken in an earlier EU funded research programme (BE95-2056) reported in references (8,9) with potential developments of this work explored in (10). However, the concept of creating a system able to fully cover the total design process and to include the concept that the teams involved are distributed has not been previously considered and is the focus for the MOB project.

本文提出的MDO方法的发展是基于航空航天部门开展的广泛研究方案。其中一些工作来自内部系统开发，以支持实际生产飞机的创建，参考文献(1)和(2)是典型的例子。其他研究的重点是开发方法，主要在概念或早期初步设计阶段(2-6)和大规模计算提供的机会中使用各种优化方法来支持MDO的应用(7)。在参考文献(8,9)中报道的早期欧盟资助的研究计划(BE95-2056)中进行了实际飞机部件的最详细应用，并在(10)中探讨了这项工作的潜在发展。然而，创建一个能够完全覆盖整个设计过程的系统的概念，并包括所涉及的团队分布的概念，这是MOB项目的重点。
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引用次数: 2
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