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Pressure and Temperature Sensitive Paints

  • Book
  • © 2021

Overview

  • Explains the physical principles of PSP and TSP
  • Describes the technical aspects of instrumentation including calibration, illumination, detection, and data/image processing
  • Discusses the measurement uncertainty of PSP and TSP
  • Describe PSP and TSP measurements in various facilities in a broad range of applications

Part of the book series: Experimental Fluid Mechanics (FLUID)

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Table of contents (11 chapters)

Keywords

About this book

This new edition describes pressure and temperature sensitive paints (PSP and TSP) in global surface pressure and temperature measurements in aerodynamics and fluid mechanics.  The book includes the latest progress in paint formulations, instrumentation, and steady and unsteady aerodynamic measurements in various facilities including low-speed, transonic, supersonic and hypersonic wind tunnels.  The updated technical aspects of PSP and TSP in the book will be useful for students and researchers in experimental aerodynamics and fluid mechanics. 

 


Authors and Affiliations

  • Department of Mechanical and Aerospace Engineering, Western Michigan University, Kalamazoo, USA

    Tianshu Liu

  • School of Aeronautics and Astronautics, Purdue University, West Lafayette, USA

    John P. Sullivan

  • Department of Aerospace Engineering, Tohoku University, Sendai, Japan

    Keisuke Asai

  • German Aerospace Center DLR, Institute of Aerodynamics and Flow Technology, Göttengen, Germany

    Christian Klein

  • Department of Mechanical Engineering, Aichi Institute of Technology, Toyota, Aichi, Japan

    Yasuhiro Egami

About the authors



Tianshu Liu is a Professor within the Department of Mechanical and Aerospace Engineering
Western Michigan University, Kalamazoo, MI; John Sullivan is a Professor in the School of Aeronautics and Astronautics, Purdue University, West Lafayette, IN; Keisuke Asai is Professor within the Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University, Sendai, Japan; and Dr. Christian Klein is with the German Aerospace Center (DLR) of the Institute of Aerodynamics and Flow Technology Experimental Methods, Göttingen, Germany.


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