Computational Design and Optimization of Supersonic Intakes
暫譯: 超音速進氣口的計算設計與優化

Sandhu, Jatinder Pal Singh, Park, Ik Soo, Ananthkrishnan, Narayan

  • 出版商: CRC
  • 出版日期: 2025-11-26
  • 售價: $5,910
  • 貴賓價: 9.5$5,615
  • 語言: 英文
  • 頁數: 174
  • 裝訂: Hardcover - also called cloth, retail trade, or trade
  • ISBN: 1032794577
  • ISBN-13: 9781032794570
  • 相關分類: 流體力學 Fluid-mechanics
  • 海外代購書籍(需單獨結帳)

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商品描述

This book offers a unique perspective on the intersection of supersonic intake design, formal optimization methods, and the use of computational fluid dynamics (CFD) for evaluating the performance of intakes. Details of the meta-model and optimization scheme, as well the CFD solvers used at each stage of the optimization process, are presented.

Additionally, for a balanced perspective, a separate chapter presents a faster, lower-fidelity alternative to RANS computation, complemented by its illustrative application to hypersonic intakes.

Key Features:

  • Discusses multi-objective design of supersonic intakes using formal optimization tools such as Kriging/MOGA.
  • Leverages advancement in CFD methods and optimization techniques for practical supersonic intake design.
  • Covers reduced-order analysis of supersonic intake.
  • Focuses on the intricate aspects of cowl design and throat shaping.
  • Explores buzz simulation using a simplified analytical model, providing valuable insights into the complex dynamics of supersonic intakes

This book is aimed at graduate students, researchers, and professionals in aircraft propulsion, intake design, and aerospace engineering.

商品描述(中文翻譯)

本書提供了一個獨特的視角,探討超音速進氣口設計、正式優化方法以及計算流體力學(CFD)在評估進氣口性能中的應用。書中詳細介紹了元模型和優化方案,以及在優化過程每個階段使用的CFD求解器。

此外,為了提供平衡的視角,另有一章介紹了一種比RANS計算更快、低保真的替代方案,並輔以其在超音速進氣口的應用示例。

主要特點:
- 討論使用正式優化工具(如Kriging/MOGA)進行超音速進氣口的多目標設計。
- 利用CFD方法和優化技術的進展,實現實用的超音速進氣口設計。
- 涵蓋超音速進氣口的降階分析。
- 專注於外殼設計和喉部成形的複雜方面。
- 探索使用簡化的分析模型進行的嗡嗡聲模擬,提供對超音速進氣口複雜動力學的寶貴見解。

本書旨在為航空推進、進氣口設計和航空航天工程的研究生、研究人員和專業人士提供參考。

作者簡介

Dr. Jatinder Pal Singh Sandhu is a senior R&D engineer at Yanxiki Tech., Pune, India. He has nearly a decade of experience in numerical computation and analysis of compressible high-speed flow. His expertise includes passive flow control of shock-wave boundary layer interaction, high-speed intakes, turbulence and transition modeling, and computational flow solver development. He was awarded a PhD by the Indian Institute of Technology Madras, India, for his work on laminar-to-turbulence transition modeling.

Dr. Ik Soo Park, an expert in propulsion and control technology for guided missiles and aircraft, currently works at the Agency for Defense Development of the Republic of Korea. With 30 years of experience in the field, he has conducted practical-oriented research, including system design control algorithms for supersonic inlet, combustion instability, rocket thrust vector, and DACS. His invaluable contributions to the development of rockets and air intake propulsion engines have led to the publication of ground-breaking research results, earning him multiple Best Paper awards. Currently residing in Daejeon, South Korea, Dr. Park actively serves as the academic director of the Korean Society of Propulsion Engineering and the Korea Aerospace System Engineering Society. He engages in academic activities through AIAA, IEEE, KSAS, and KSPE. Moreover, Dr. Park maintains regular exchanges with scholars from over 20 renowned research institutes worldwide, conducting international joint research and fostering continuous collaboration in related fields.

Dr Narayan Ananthkrishnan is an Independent Consultant presently based out of Mumbai (India) with nearly 30 years experience in academia and industry in multi-disciplinary research and development across a wide spectrum from Flight Dynamics & Control to Airplane Aerodynamics to Combustion Systems. Over the past decade, he has largely worked with businesses in the Mumbai/Pune area and Bangalore in India, and in Seoul and Daejeon, South Korea, and with a few select academic institutes. His recent work has focused on the broad area of Aerospace Systems Design & Integration with emphasis on Multidisciplinary Optimization and Air-breathing Propulsion Systems. He has previously served on the faculty of Aerospace Engineering at the Indian Institute of Technology, IIT Bombay at Mumbai, India, and as a Visiting Faculty Member at the California Institute of Technology at Pasadena, CA, USA. He received the "Excellence in Teaching" award at IIT Bombay in the year 2000. He has authored two textbooks (with NK Sinha), Elementary Flight Dynamics with an Introduction to Bifurcation and Continuation Methods, published by CRC Press, Taylor & Francis (2014, 2nd ed. in 2022, Chinese ed. in 2022) and Advanced Flight Dynamics with Elements of Flight Control, also published by CRC Press, Taylor & Francis (2017). He has also written an e-book on Airplane Systems, Design, and Operations. He received his education in Aerospace Engineering at the Indian Institutes of Technology, majoring in Flight Mechanics & Control, Aerodynamics, Aircraft Design, and Nonlinear Systems. He is an Associate Fellow at American Institute of Aeronautics & Astronautics (AIAA) and has served a term as a member of the AIAA Atmospheric Flight Mechanics Technical Committee.

作者簡介(中文翻譯)

Dr. Jatinder Pal Singh Sandhu 是印度浦那的 Yanxiki Tech. 的資深研發工程師。他在可壓縮高速流的數值計算和分析方面擁有近十年的經驗。他的專業領域包括衝擊波邊界層互動的被動流控制、高速進氣口、湍流和過渡建模,以及計算流動求解器的開發。他因在層流到湍流過渡建模方面的研究而獲得印度理工學院馬德拉斯分校的博士學位。

Dr. Ik Soo Park 是導引飛彈和飛機推進與控制技術的專家,目前在韓國國防開發局工作。他在該領域擁有30年的經驗,進行了以實用為導向的研究,包括超音速進氣口的系統設計控制演算法、燃燒不穩定性、火箭推力向量和DACS。他對火箭和空氣進氣推進引擎的發展做出了寶貴的貢獻,並發表了開創性的研究成果,獲得多項最佳論文獎。Dr. Park 目前居住在韓國大田,積極擔任韓國推進工程學會和韓國航空系統工程學會的學術主任。他通過 AIAA、IEEE、KSAS 和 KSPE 參與學術活動。此外,Dr. Park 與全球20多個知名研究機構的學者保持定期交流,進行國際聯合研究並促進相關領域的持續合作。

Dr. Narayan Ananthkrishnan 是一位獨立顧問,目前居住在印度孟買,擁有近30年的學術和產業經驗,專注於從飛行動力學與控制到飛機氣動力學再到燃燒系統的多學科研究與開發。在過去十年中,他主要與印度孟買/浦那地區和班加羅爾的企業,以及韓國首爾和大田的一些選定學術機構合作。他最近的工作集中在航空系統設計與整合的廣泛領域,強調多學科優化和空氣呼吸推進系統。他曾在印度理工學院孟買分校的航空工程系任教,並擔任美國加州理工學院的訪問教員。他於2000年在印度理工學院孟買分校獲得「教學卓越獎」。他與 NK Sinha 共同撰寫了兩本教科書,分別是由 CRC Press、Taylor & Francis 出版的 Elementary Flight Dynamics with an Introduction to Bifurcation and Continuation Methods(2014年,2022年第二版,2022年中文版)和 Advanced Flight Dynamics with Elements of Flight Control(2017年)。他還撰寫了一本關於飛機系統、設計和操作的電子書。他在印度理工學院接受航空工程教育,主修飛行力學與控制、氣動力學、飛機設計和非線性系統。他是美國航空航天學會(AIAA)的副研究員,並曾擔任 AIAA 大氣飛行力學技術委員會的成員。