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Hypersonic Curved Compression Inlet and Its Inverse Design

  • Kunyuan Zhang
Book

Part of the Advanced Topics in Science and Technology in China book series (ATSTC, volume 56)

About this book

Introduction

This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic–hypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the author’s research at the Deutsches Zentrum fur Luft- und Raumfahrt (DLR SM-ES) in the early 1990s. This book introduces the research history, working characteristics, performance calculation and aerodynamic configuration design method of this compression mode in detail. It also describes method of estimating the minimum drag in inlet and drag reduction effect of curved compression and proposes a new index for evaluating unit area compression efficiency of the inlet. Further, it reviews the relevant recent research on curved compression. As such it is a valuable resource for students, researchers and scientists in the fields of hypersonic propulsion and aeronautics.

Keywords

hypersonic propulsion hypersonic inlet curved shock compression curved compression surface inverse design supersonic inlet

Authors and affiliations

  • Kunyuan Zhang
    • 1
  1. 1.College of Energy and Power EngineeringNanjing University of Aeronautics and AstronauticsNanjingChina

Bibliographic information

  • DOI https://doi.org/10.1007/978-981-15-0727-4
  • Copyright Information Zhejiang University Press and Springer Nature Singapore Pte Ltd. 2020
  • Publisher Name Springer, Singapore
  • eBook Packages Physics and Astronomy
  • Print ISBN 978-981-15-0726-7
  • Online ISBN 978-981-15-0727-4
  • Series Print ISSN 1995-6819
  • Series Online ISSN 1995-6827
  • Buy this book on publisher's site