Pressure and Temperature Sensitive Paints PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Pressure and Temperature Sensitive Paints PDF full book. Access full book title Pressure and Temperature Sensitive Paints by Tianshu Liu. Download full books in PDF and EPUB format.
Author: Tianshu Liu
Publisher: Springer Science & Business Media
ISBN: 3540266445
Category : Technology & Engineering
Languages : en
Pages : 331
Get Book Here
Book Description
Luminescent molecule sensors, called pressure-sensitive paint (PSP) and temperature-sensitive paint (TSP), measure factors essential for understanding the aerodynamic performance and heat transfer characteristics of flight vehicles. They provide a powerful tool for experimental aerodynamicists to obtain a deeper understanding of the rich physical phenomena in complex flows around a flight vehicle. This book helps the reader to understand the physics and chemistry and the capabilities of PSP and TSP. It provides an overview of the wide scope of applications and explains the system requirements for using these sensors. The book also includes an extensive table of properties of PTP and TSP. As such, it is a thorough and up-to-date coverage of the underlying physics and applications of luminescent molecules designed for global pressure and temperature mapping
Author: Tianshu Liu
Publisher: Springer Science & Business Media
ISBN: 3540266445
Category : Technology & Engineering
Languages : en
Pages : 331
Get Book Here
Book Description
Luminescent molecule sensors, called pressure-sensitive paint (PSP) and temperature-sensitive paint (TSP), measure factors essential for understanding the aerodynamic performance and heat transfer characteristics of flight vehicles. They provide a powerful tool for experimental aerodynamicists to obtain a deeper understanding of the rich physical phenomena in complex flows around a flight vehicle. This book helps the reader to understand the physics and chemistry and the capabilities of PSP and TSP. It provides an overview of the wide scope of applications and explains the system requirements for using these sensors. The book also includes an extensive table of properties of PTP and TSP. As such, it is a thorough and up-to-date coverage of the underlying physics and applications of luminescent molecules designed for global pressure and temperature mapping
Author: Tianshu Liu
Publisher: Springer Nature
ISBN: 3030680568
Category : Technology & Engineering
Languages : en
Pages : 552
Get Book Here
Book Description
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.
Author: National Aeronaut Administration (Nasa)
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Get Book Here
Book Description
This report documents the Pressure and Temperature Sensitive Paint Field System that is used to provide global surface pressure and temperature measurements on models tested in Langley wind tunnels. The system was developed and is maintained by Global Surface Measurements Team personnel of the Data Acquisition and Information Management Branch in the Research Facilities Services Competency. Descriptions of the system hardware and software are presented and operational procedures are detailed. Sprinkle, Danny R. and Obara, Clifford J. and Amer, Tahani R. and Faulcon, Nettie D. and Carmine, Michael T. and Burkett, Cecil G. and Pritchard, Daniel W. and Oglesby, Donald M. Langley Research Center; NASA Headquarters NASA/TM-2004-213020, L-183774 PRESSURE SENSITIVE PAINTS; TEMPERATURE SENSITIVE PAINTS; WIND TUNNELS; ELECTRONIC EQUIPMENT; PHOTOMETRY; SPECTROPHOTOMETRY; FLOW VISUALIZATION; DATA ACQUISITION; COMPUTER PROGRAMS
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781724007933
Category : Science
Languages : en
Pages : 32
Get Book Here
Book Description
Luminescent molecular probes imbedded in a polymer binder form a temperature or pressure paint. On excitation by light of the proper wavelength, the luminescence, which is quenched either thermally or by oxygen, is detected by a camera or photodetector. From the detected luminescent intensity, temperature and pressure can be determined. The basic photophysics, calibration, accuracy and time response of luminescent paints is described followed by applications in wind tunnels and in rotating machinery. Sullivan, John Ames Research Center
Author: Kirk S. Schanze
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: M. A. Woodmansee
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: Judith A. Muller
Publisher:
ISBN: 9781423535935
Category :
Languages : en
Pages : 88
Get Book Here
Book Description
In order to obtain quantitative surface pressure measurements of a transonic compressor rotor using pressure sensitive paint (PSP), the temperature dependence of the paint must be taken into consideration. In the present study, a calibration chamber was built and instrumented such that pressure and temperature could be controlled independently. Photodiodes were used to measure the intensity of light emitted by the PSP. An acquisition program was developed to record the necessary calibration data to obtain an analytical representation of the luminescent response of the pressure-sensitive paint over a range of pressures and temperatures characteristic of transonic fans.
Author: Matthias I. J. Stich
Publisher:
ISBN:
Category :
Languages : en
Pages : 246
Get Book Here
Book Description
Author: Kelly R. Navarra
Publisher:
ISBN: 9781423549949
Category :
Languages : en
Pages : 92
Get Book Here
Book Description
A new pressure measurement technique that employs the tools of molecular spectroscopy has recently received considerable attention in the community. Measurements are made via oxygen-sensitive molecules attached to the surface of interest as a coating, or paint. The pressure-sensitive paint (PSP) technique is now commonly used in stationary wind tunnel tests; this thesis presents extension of the technique to advanced turbomachinery applications. New pressure- and temperature-sensitive paints (TSPs) have been developed for application to a state-of-the-art compressor where pressures up to 2 atm and surface temperatures to 140 deg C are expected for the first stage rotor. PSP and TSP data images have been acquired from the suction surface of the first- stage rotor at 85 percent of the correct design speed for the compressor peak efficiency condition. The shock structure is clearly visible in the pressure image, and visual comparison to the corresponding computer prediction shows quantitative pressures similar to the PSP data. The measurement error is estimated to range from 0.36 kPa in low pressure regions to 4 kPa in high pressure regions.
Author: Peter D. Baumann
Publisher:
ISBN: 9781423556213
Category :
Languages : en
Pages : 104
Get Book Here
Book Description
In the development of a surface pressure measurement system for transonic compressor rotors, it has been shown that Pressure Sensitive Paint (PSP) is also temperature dependent. In the present study, the sensitivities to pressure and temperature were examined experimentally using an electronically- gated, intensified Charged- Coupled-Device (CCD) video camera, frame-grabber software and an eight-inch diameter calibration chamber. Using a signal generator, in a procedure that matched the requirements of the rotor application, multiple low-intensity-level camera exposures were integrated and captured to produce a single usable image. Ten captured images were averaged to increase the image's signal-to-noise ratio and the result was used to produce an image ratio with respect to a static (ambient pressure/temperature) reference condition. Calibration tests of constant temperature/variable pressure and constant pressure/variable temperature were completed. The results were then compared with data obtained using the same paint and an automated, single- exposure calibration procedure at NASA Ames Research Center. It was shown that the calibration data could be used to derive the static pressure field produced over a high-speed test rotor using PSP and the same image-capture system used in the calibration. In preparation for a bench test of the procedure, a uniform- stress, high-speed test rotor disk, fitted with a shock generator was driven at speeds in excess of 30,000 RPM. Recommendations are made toward the goal of obtaining quantitative pressure measurements on transonic compressor rotors.
