A Wind Tunnel Test Demonstrating the Capabilities of Pressure Sensitive Paint

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ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis A Wind Tunnel Test Demonstrating the Capabilities of Pressure Sensitive Paint by :

Download or read book A Wind Tunnel Test Demonstrating the Capabilities of Pressure Sensitive Paint written by and published by . This book was released on 1995 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: A comparison of a pressure sensitive paint (PSP) developed at Arnold Engineering Development Center (AEDC) with a PSP developed in Russia was performed in the AEDC Propulsion Wind Tunnel l6T. A Generic Wall Interference Model, similar to an old AEDC model used to study wall interference effects, was fabricated at the Central Aerohydrodynamics Institute (TsAGI) in Zhukovsky, Russia. The model has been tested in the TsAGI T-128 wind tunnel and was sent to AEDC with the balance and sting support hardware for the 16T test. The AEDC PSP and Russian PSP were applied to separate wings of the model. Conventional pressure, PSP, and force data were acquired simultaneously at Mach numbers 0.60, 0.85, and 0.95 while angle of attack was varied from - 10 to 10 deg. The stagnation pressure and temperature was also varied to permit evaluations of the pressure and temperature sensitivity of each paint.

Demonstration Test of Pressure Sensitive Paint in the AEDC 16-ft Transonic Wind Tunnel Using the TST Model

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Demonstration Test of Pressure Sensitive Paint in the AEDC 16-ft Transonic Wind Tunnel Using the TST Model by : M. E. Sellers

Download or read book Demonstration Test of Pressure Sensitive Paint in the AEDC 16-ft Transonic Wind Tunnel Using the TST Model written by M. E. Sellers and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Demonstrations of a Pressure Sensitive Paint Data System in the AEDC Propulsion Wind Tunnel 16T.

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ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Demonstrations of a Pressure Sensitive Paint Data System in the AEDC Propulsion Wind Tunnel 16T. by :

Download or read book Demonstrations of a Pressure Sensitive Paint Data System in the AEDC Propulsion Wind Tunnel 16T. written by and published by . This book was released on 1995 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: A prototype Pressure Sensitive Paint (PS P) data system was assembled to demonstrate the capability to acquire and process surface pressure date using PSP in the AFDC Propulsion Wind Tunnel 16T. The first test was preformed on a 1/10-scale model of the Dornier Alpha Jet with a Transonic Technology (TST) Wing to obtain PSP data for comparison with conventional pressure measurements and Computational Fluid Dynamics (CFD) results. The second test was performed on a 15-percent scale model of the F-18 ElF to obtain PSP data on the upper and lower surface of the F-18 horizontal tail for comparison with conventional pressure measurements. Also, the PSP data were integrated to obtain loads on the horizontal tail for comparison with conventional pressure-integrated and balance-measured loads. A paint formulation developed at AEDC was used in the tests. Some of the unique features of the paint are discussed, and details of the data acquisition and reduction system are presented. The data system was controlled by the facility computer, which acquired PSP data automatically. The digitized images were processed to obtain qualitative images of the surface pressure distribution within minutes of acquisition. The images were processed further after the tests to obtain quantitative pressure data. Comparisons with measured pressure data, CFD solutions (TST only), and measured and integrated loads (F-18 only) are presented.

Lecture series

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ISBN 13 :
Total Pages : 280 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Lecture series by :

Download or read book Lecture series written by and published by . This book was released on 2001 with total page 280 pages. Available in PDF, EPUB and Kindle. Book excerpt:

21st AIAA Advanced Measurement and Ground Testing Technology Conference: 00-2528 - 00-2700

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ISBN 13 :
Total Pages : 446 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 21st AIAA Advanced Measurement and Ground Testing Technology Conference: 00-2528 - 00-2700 by :

Download or read book 21st AIAA Advanced Measurement and Ground Testing Technology Conference: 00-2528 - 00-2700 written by and published by . This book was released on 2000 with total page 446 pages. Available in PDF, EPUB and Kindle. Book excerpt:

18th AIAA Aerospace Ground Testing Conference

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ISBN 13 :
Total Pages : 428 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 18th AIAA Aerospace Ground Testing Conference by :

Download or read book 18th AIAA Aerospace Ground Testing Conference written by and published by . This book was released on 1994 with total page 428 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds

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ISBN 13 :
Total Pages : 170 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds by : John E. Lamar

Download or read book Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds written by John E. Lamar and published by . This book was released on 2001 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt: Geometrical, flight, computational fluid dynamics (CFD), and wind-tunnel studies for the F-16XL-1 airplane are summarized over a wide range of test conditions. Details are as follows: (1) For geometry, the upper surface of the airplane and the numerical surface description compare reasonably well. (2) For flight, CFD, and wind-tunnel surface pressures, the comparisons are generally good at low angles of attack at both subsonic and transonic speeds; however, local differences are present. In addition, the shock location at transonic speeds from wind-tunnel presure contours is near the aileron hinge line and generally is in correlative agreement with flight results.

NASA Technical Paper

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ISBN 13 :
Total Pages : 170 pages
Book Rating : 4.F/5 ( download)

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Download or read book NASA Technical Paper written by and published by . This book was released on with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Application of Pressure-Sensitive Paint to Ice-Accreted Wind Tunnel Models

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ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Application of Pressure-Sensitive Paint to Ice-Accreted Wind Tunnel Models by : Timothy J. Bencic

Download or read book Application of Pressure-Sensitive Paint to Ice-Accreted Wind Tunnel Models written by Timothy J. Bencic and published by . This book was released on 2000 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Departments of Veterans Affairs and Housing and Urban Development, and Independent Agencies Appropriations for 1996

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ISBN 13 :
Total Pages : 908 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Departments of Veterans Affairs and Housing and Urban Development, and Independent Agencies Appropriations for 1996 by : United States. Congress. House. Committee on Appropriations. Subcommittee on VA, HUD, and Independent Agencies

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NASA Technical Memorandum

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ISBN 13 :
Total Pages : 458 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Memorandum by :

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1992 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Capabilities for the Future

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Publisher : National Academies Press
ISBN 13 : 0309153514
Total Pages : 112 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Capabilities for the Future by : National Research Council

Download or read book Capabilities for the Future written by National Research Council and published by National Academies Press. This book was released on 2010-06-13 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: Over the past 5 years or more, there has been a steady and significant decrease in NASA's laboratory capabilities, including equipment, maintenance, and facility upgrades. This adversely affects the support of NASA's scientists, who rely on these capabilities, as well as NASA's ability to make the basic scientific and technical contributions that others depend on for programs of national importance. The fundamental research community at NASA has been severely impacted by the budget reductions that are responsible for this decrease in laboratory capabilities, and as a result NASA's ability to support even NASA's future goals is in serious jeopardy.

International Aerospace Abstracts

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ISBN 13 :
Total Pages : 1032 pages
Book Rating : 4.F/5 ( download)

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Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 1032 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Pressure and Temperature Sensitive Paints

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Publisher : Springer Science & Business Media
ISBN 13 : 9783540222415
Total Pages : 348 pages
Book Rating : 4.2/5 (224 download)

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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 2005 with total page 348 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

The NASA Scientific and Technical Information Program

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ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis The NASA Scientific and Technical Information Program by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Program

Download or read book The NASA Scientific and Technical Information Program written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Program and published by . This book was released on 1993 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

AIAA Journal

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ISBN 13 :
Total Pages : 1358 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis AIAA Journal by : American Institute of Aeronautics and Astronautics

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NASA Aeronautics

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ISBN 13 :
Total Pages : 80 pages
Book Rating : 4.:/5 (31 download)

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Download or read book NASA Aeronautics written by and published by . This book was released on 1992 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: