Drag Reduction by Shock and Boundary Layer Control : Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design Vol.80) (2002. XX, 449 p. w. numerous graphs and figs. 24,5 cm)

個数:

Drag Reduction by Shock and Boundary Layer Control : Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design Vol.80) (2002. XX, 449 p. w. numerous graphs and figs. 24,5 cm)

  • 在庫がございません。海外の書籍取次会社を通じて出版社等からお取り寄せいたします。
    通常6~9週間ほどで発送の見込みですが、商品によってはさらに時間がかかることもございます。
    重要ご説明事項
    1. 納期遅延や、ご入手不能となる場合がございます。
    2. 複数冊ご注文の場合、分割発送となる場合がございます。
    3. 美品のご指定は承りかねます。

  • 提携先の海外書籍取次会社に在庫がございます。通常3週間で発送いたします。
    重要ご説明事項
    1. 納期遅延や、ご入手不能となる場合が若干ございます。
    2. 複数冊ご注文の場合、分割発送となる場合がございます。
    3. 美品のご指定は承りかねます。
  • 【入荷遅延について】
    世界情勢の影響により、海外からお取り寄せとなる洋書・洋古書の入荷が、表示している標準的な納期よりも遅延する場合がございます。
    おそれいりますが、あらかじめご了承くださいますようお願い申し上げます。
  • ◆画像の表紙や帯等は実物とは異なる場合があります。
  • ◆ウェブストアでの洋書販売価格は、弊社店舗等での販売価格とは異なります。
    また、洋書販売価格は、ご注文確定時点での日本円価格となります。
    ご注文確定後に、同じ洋書の販売価格が変動しても、それは反映されません。
  • 製本 Hardcover:ハードカバー版/ページ数 450 p.
  • 商品コード 9783540433170

Full Description

The survival of the Aeronautical Industries of Europe in the highly competitive World Aviation Market is strongly dependent on such factors as time-to-market of a new or derivative aircraft and on its manufacturing costs but also on the achievement of a competitive technological advantage by which an increased market share can be gained. Recognizing this, cooperative research is continuously encouraged and co-financed by the European Union in order to strengthen the scientific and technological base of the Aeronautical Industries thus providing - among others - the technological edge needed for survival. Corresponding targets of research within Area 3, Technologies for Transport Means, and here in particular Area 3A, Aeronautics Technologies, of the Industrial and Materials Technologies Program ( Brite -EuRam III, 1994 -1998) have been identified to be aircraft efficiency, cost effectiveness and environmental impact. Concerning aircraft efficiency - relevant to the present research - a reduction in aircraft drag of 10%, a reduction in aircraft fuel consumption of 30%, and a reduction in airframe, engine and system weight of 20% are envisaged. Meeting these objectives has, of course, also a strong positive impact on the environment.

Contents

Introduction.- The EUROSHOCK II Project.- Modeling of Active Control Phenomena.- Numerical Simulation of Airfoil and Wing Flow with Control.- Airfoil and Sheared-Wing Experiments with and Without Control.- Benefits of Control Application to Aircraft Wings/Aircraft.- Assessment of Shock and Boundary Layer Control - A Summary.- Overall Conclusions and Future Work.- Introduction to the Individual Contributions.- Study of Control Devices Applied to a Transonic Shock Wave/Boundary Layer Interaction.- Hybrid and Active Control of Shock Wave - Turbulent Boundary Layer Interaction and Perforated Plate Transpiration Flow.- Active Control of Swept Shock Wave/Boundary Layer Interactions.- Numerical Investigation of Active Shock Wave and Boundary Layer Control on Airfoils and Sheared Wings.- Boundary Layer Coupling to Predict Steady and Unsteady Transonic Flows Past an Airfoil with and Without Shock Control.- 2D Numerical Investigations of Shock and Boundary Layer Control Techniques.