Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Use Of Pressure Sensitive Paint For Diagnostics In Turbomachinery Flows With Shocks Nasa Tm 2001 211111 Mar 8 2002
Download Use Of Pressure Sensitive Paint For Diagnostics In Turbomachinery Flows With Shocks Nasa Tm 2001 211111 Mar 8 2002 full books in PDF, epub, and Kindle. Read online Use Of Pressure Sensitive Paint For Diagnostics In Turbomachinery Flows With Shocks Nasa Tm 2001 211111 Mar 8 2002 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis USE OF PRESSURE SENSITIVE PAINT FOR DIAGNOSTICS IN TURBOMACHINERY FLOWS WITH SHOCKS... NASA/TM-2001-211111... MAR. 8, 2002 by :
Download or read book USE OF PRESSURE SENSITIVE PAINT FOR DIAGNOSTICS IN TURBOMACHINERY FLOWS WITH SHOCKS... NASA/TM-2001-211111... MAR. 8, 2002 written by and published by . This book was released on 2002 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Use of Pressure Sensitive Paint for Diagnostics in Turbomachinery Flows With Shocks by :
Download or read book Use of Pressure Sensitive Paint for Diagnostics in Turbomachinery Flows With Shocks written by and published by . This book was released on 2001 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Use of Pressure Sensitive Paint for Diagnostics in Turbomachinery Flows with Shocks... NASA by :
Download or read book Use of Pressure Sensitive Paint for Diagnostics in Turbomachinery Flows with Shocks... NASA written by and published by . This book was released on 1998 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressure and Temperature Sensitive Paints by : Tianshu Liu
Download or read book Pressure and Temperature Sensitive Paints written by Tianshu Liu and published by Springer Science & Business Media. This book was released on 2006-01-06 with total page 331 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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
Book Synopsis Pressure and Temperature Sensitive Paints by : Tianshu Liu
Download or read book Pressure and Temperature Sensitive Paints written by Tianshu Liu and published by Springer Nature. This book was released on 2021-07-31 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System by : Danny R. Sprinkle
Download or read book Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System written by Danny R. Sprinkle and published by . This book was released on 2001 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes the NASA Langley 16-Ft. Transonic Tunnel Pressure Sensitive Paint (PSP) system and presents results of a test conducted June 22-23, 2000 in the tunnel to validate the PSP system. The PSP system provides global surface pressure measurements on wind tunnel models. The system was developed and installed by PSP Team personnel of the Instrumentation Systems Development Branch and the Advanced Measurement and Diagnostics Branch. A discussion of the results of the validation test follows a description of the system and a description of the test.
Book Synopsis Pressure-sensitive Paint Investigation for Turbomachinery Application by : K. Sabroske
Download or read book Pressure-sensitive Paint Investigation for Turbomachinery Application written by K. Sabroske and published by . This book was released on 1995 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine and Aeroengine Congress and Exposition, Houston, Texas - June 5-8, 1995.
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781721674749 Total Pages :28 pages Book Rating :4.6/5 (747 download)
Book Synopsis Water-Based Pressure Sensitive Paint by : National Aeronautics and Space Administration (NASA)
Download or read book Water-Based Pressure Sensitive Paint written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-21 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Preparation and performance of a water-based pressure sensitive paint (PSP) is described. A water emulsion of an oxygen permeable polymer and a platinum porphyrin type luminescent compound were dispersed in a water matrix to produce a PSP that performs well without the use of volatile, toxic solvents. The primary advantages of this PSP are reduced contamination of wind tunnels in which it is used, lower health risk to its users, and easier cleanup and disposal. This also represents a cost reduction by eliminating the need for elaborate ventilation and user protection during application. The water-based PSP described has all the characteristics associated with water-based paints (low toxicity, very low volatile organic chemicals, and easy water cleanup) but also has high performance as a global pressure sensor for PSP measurements in wind tunnels. The use of a water-based PSP virtually eliminates the toxic fumes associated with the application of PSPs to a model in wind tunnels. Oglesby, Donald M. and Ingram, JoAnne L. and Jordan, Jeffrey D. and Watkins, A. Neal and Leighty, Bradley D. Langley Research Center NASA/TM-2004-213268, L-18349
Book Synopsis Pressure-Sensitive Paint Measurement Technique Development for Turbomachinery Application by : Kevin J. Quinn
Download or read book Pressure-Sensitive Paint Measurement Technique Development for Turbomachinery Application written by Kevin J. Quinn and published by . This book was released on 1997-12-01 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure-sensitive paint measurement on a transonic compressor rotor required the prior development of phase-locked cumulative imaging using a disk- rotor driven by a high-speed Hamilton-Standard turbine as a developmental test- bed. The turbine was installed in a protective housing in the Gas Dynamics Laboratory and connected to an 8000 cu ft, 300 psi air supply. An hydraulic pump provided bearing lubrication. A once per revolution trigger signal was produced from a light-emitting diode and PIN photodiode pair. The imaging system consisted of an intensified CCD video camera externally triggered by the 1/rev signal via a waveform shaping circuit designed for the present application. Images were captured at camera gate speeds calculated to eliminate pixel blur and image integration times were varied to optimize image intensity and spatial resolution. Structural and modal analyses of the disk-rotor were conducted and a simplified numerical model of the flow was computed. Ratioed, colored images were produced for wheel speeds to 20,000 RPM. The effect of the radially varying stagnation temperature was evident, underscoring the importance of quantifying and accounting for the PSP temperature sensitivity so that quantitative pressure data may be obtained. Recommendations for a follow-on program are reported.