Future Space-Transport-System Components under High Thermal and Mechanical Loads : Results from the DFG Collaborative Research Center TRR40 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design)

個数：

Future Space-Transport-System Components under High Thermal and Mechanical Loads : Results from the DFG Collaborative Research Center TRR40 (Notes on Numerical Fluid Mechanics and Multidisciplinary Design)

Adams, Nikolaus A. (EDT)/ Schröder, Wolfgang (EDT)/ Radespiel, Rolf (EDT)

ウェブストア価格 ¥22,455（本体¥20,414）
Springer Nature Switzerland AG（2021/10発売）
外貨定価 US$ 109.99
ポイント 204pt

オンデマンド(OD/POD)版です。キャンセルは承れません。

【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 Paperback:紙装版/ペーパーバック版／ページ数 419 p.
言語 ENG
商品コード 9783030538491

Full Description

This open access book presents the findings of Collaborative Research Center Transregio 40 (TRR40), initiated in July 2008 and funded by the German Research Foundation (DFG). Gathering innovative design concepts for thrust chambers and nozzles, as well as cutting-edge methods of aft-body flow control and propulsion-component cooling, it brings together fundamental research undertaken at universities, testing carried out at the German Aerospace Center (DLR) and industrial developments from the ArianeGroup. With a particular focus on heat transfer analyses and novel cooling concepts for thermally highly loaded structures, the book highlights the aft-body flow of the space transportation system and its interaction with the nozzle flow, which are especially critical during the early phase of atmospheric ascent. Moreover, it describes virtual demonstrators for combustion chambers and nozzles, and discusses their industrial applicability. As such, it is a timely resource for researchers, graduate students and practitioners.

Collaborative Research for Future Space Transportation Systems.- Innovative Cooling for Rocket Combustion Chambers.- Film Cooling in Rocket Nozzle.- Heat Transfer in Pulsating Flow and its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators.- Eﬀects of a Launcher's External Fow on a Dual-Bell Nozzle Flow.- Interaction of Wake and Propulsive Jet Flow of a Generic Space Launcher.- Numerical Analysis of the Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle.