Fundamental Concepts of Liquid-Propellant Rocket Engines
暫譯: 液體推進火箭引擎的基本概念

de Iaco Veris, Alessandro

Fundamental Concepts of Liquid-Propellant Rocket Engines
  • 出版商: Springer
  • 出版日期: 2020-09-27
  • 售價: $2,660
  • 貴賓價: 9.5 折 $2,527
  • 語言: 英文
  • 頁數: 747
  • 裝訂: Hardcover - also called cloth, retail trade, or trade
  • ISBN: 3030547035
  • ISBN-13: 9783030547035
  • 相關分類: 動力學 Dynamics

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商品描述

This book is intended for students and engineers who design and develop liquid-propellant rocket engines, offering them a guide to the theory and practice alike. It first presents the fundamental concepts (the generation of thrust, the gas flow through the combustion chamber and the nozzle, the liquid propellants used, and the combustion process) and then qualitatively and quantitatively describes the principal components involved (the combustion chamber, nozzle, feed systems, control systems, valves, propellant tanks, and interconnecting elements). The book includes extensive data on existing engines, typical values for design parameters, and worked-out examples of how the concepts discussed can be applied, helping readers integrate them in their own work. Detailed bibliographical references (including books, articles, and items from the "gray literature") are provided at the end of each chapter, together with information on valuable resources that can be found online. Given its scope, the book will be of particular interest to undergraduate and graduate students of aerospace engineering.


商品描述(中文翻譯)

本書旨在為設計和開發液體推進劑火箭引擎的學生和工程師提供理論與實踐的指南。書中首先介紹基本概念（推力的產生、氣體在燃燒室和噴嘴中的流動、所使用的液體推進劑以及燃燒過程），然後定性和定量地描述涉及的主要組件（燃燒室、噴嘴、供料系統、控制系統、閥門、推進劑儲罐和連接元件）。本書包含現有引擎的廣泛數據、設計參數的典型值以及如何應用所討論概念的具體範例，幫助讀者將其整合到自己的工作中。每章末尾提供詳細的參考文獻（包括書籍、文章和「灰色文獻」中的項目），以及可以在線找到的有價值資源的信息。考慮到其範疇，本書將特別吸引航空航天工程的本科生和研究生。

作者簡介

Alessandro de Iaco Veris holds degrees in civil engineering and aerospace engineering, both from the University of Rome. He has also completed specialist training, including a high-level professional course on "Projet, calcul et emploi des fusées spatiales" at the Ecole Nationale Supérieure de l'Aéronautique et de l'Espace (ENSAE) and a course on "Dynamics of Controlled Structures" at Massachusetts Institute of Technology (MIT). He is a strong proponent of the application of mathematics for practical purposes and in particular for the solution of problems arising in engineering. His expertise is in the fields of mathematical models and numerical methods for aerodynamics, space flight mechanics, system studies, and mission analysis. His professional interests include numerical integration methods used to predict the motion of space vehicles and Earth satellites subject to perturbations.

作者簡介(中文翻譯)

Alessandro de Iaco Veris 擁有羅馬大學的土木工程和航空航天工程學位。他還完成了專業培訓，包括在法國國立航空航天學院（Ecole Nationale Supérieure de l'Aéronautique et de l'Espace, ENSAE）進行的高級專業課程「火箭的設計、計算與應用」（Projet, calcul et emploi des fusées spatiales），以及在麻省理工學院（Massachusetts Institute of Technology, MIT）修習的「受控結構的動力學」（Dynamics of Controlled Structures）課程。他強烈支持數學在實際應用中的使用，特別是在解決工程問題方面。他的專業領域包括數學模型和數值方法，應用於空氣動力學、太空飛行力學、系統研究和任務分析。他的專業興趣包括用於預測受擾動影響的太空載具和地球衛星運動的數值積分方法。

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