Facilities and Techniques for Aerodynamic Testing at Transonic Speeds and High Reynolds Number

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ISBN 13 :
Total Pages : 450 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis Facilities and Techniques for Aerodynamic Testing at Transonic Speeds and High Reynolds Number by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel

Download or read book Facilities and Techniques for Aerodynamic Testing at Transonic Speeds and High Reynolds Number written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel and published by . This book was released on 1971 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt: In September 1968, the FDP of AGARD held a specialists' meeting in Paris on transonic aerodynamics, in recognition of the fact that the absence of adequate theoretical methods and wind-tunnels of high enough Reynolds number had already led to costly shortcomings in the transonic performance of certain combat and transport aircraft. Since projected aerospace systems, military, civil and space-oriented, would involve flight at Reynolds number of up to 100 million, the FDP undertook an examination of the requirements of NATO nations for wind tunnel facilities for testing large models at high Reynolds numbers.

Aerodynamic Testing at High Reynolds Numbers and Transonic Speeds

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Publisher :
ISBN 13 :
Total Pages : 8 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Aerodynamic Testing at High Reynolds Numbers and Transonic Speeds by : D. Küchemann

Download or read book Aerodynamic Testing at High Reynolds Numbers and Transonic Speeds written by D. Küchemann and published by . This book was released on 1971 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt: As a contribution to a 1971 NATO seminar on aerodynamical testing facilities, a brief report is given on the outcome of a specialists' meeting organized by the fluid dynamics panel of AGARD and held at Gottingen. The best technical advice available within AGARD leads to the conclusion that one or several large new windtunnels would contribute immensely to the effectiveness of a large number of aerospace systems now planned or contemplated within the NATO nations.

Cryogenic Wind Tunnels for High Reynolds Number Testing

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ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Cryogenic Wind Tunnels for High Reynolds Number Testing by :

Download or read book Cryogenic Wind Tunnels for High Reynolds Number Testing written by and published by . This book was released on 1986 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamics of the Model Airplane: Airfoil measurements

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ISBN 13 :
Total Pages : 218 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis Aerodynamics of the Model Airplane: Airfoil measurements by : Franz Wilhelm Schmitz

Download or read book Aerodynamics of the Model Airplane: Airfoil measurements written by Franz Wilhelm Schmitz and published by . This book was released on 1967 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 958 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1975 with total page 958 pages. Available in PDF, EPUB and Kindle. Book excerpt:

High Speed Problems of Aircraft and Experimental Methods

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Publisher : Princeton University Press
ISBN 13 : 140087503X
Total Pages : 1021 pages
Book Rating : 4.4/5 (8 download)

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Book Synopsis High Speed Problems of Aircraft and Experimental Methods by : Allen F. Donovan

Download or read book High Speed Problems of Aircraft and Experimental Methods written by Allen F. Donovan and published by Princeton University Press. This book was released on 2015-12-08 with total page 1021 pages. Available in PDF, EPUB and Kindle. Book excerpt: Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 328 pages
Book Rating : 4.:/5 (3 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flow at Ultra-High Reynolds and Rayleigh Numbers

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Publisher : Springer Science & Business Media
ISBN 13 : 1461222303
Total Pages : 483 pages
Book Rating : 4.4/5 (612 download)

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Book Synopsis Flow at Ultra-High Reynolds and Rayleigh Numbers by : Russell J. Donnelly

Download or read book Flow at Ultra-High Reynolds and Rayleigh Numbers written by Russell J. Donnelly and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 483 pages. Available in PDF, EPUB and Kindle. Book excerpt: Scientists have learned to use liquid and gaseous helium to overcome the limitations imposed by the usual wind and water tunnels for testing the performance of aircraft or the behavior of the atmosphere. This book covers fundamental studies of the turbulence problem, practical applications of turbulence, superfluid turbulence, cryogenic turbulence research, and new types of miniature flow instrumentation, all which are crucial for high Reynolds number research. This state-of-the-art presentation will interest physicists in fluid dynamics, engineers working with turbulent flows, and naval and aerospace engineers testing realistic parameter ranges.

High Reynolds Number Tests of a NASA SC(3)-0712(B) Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

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ISBN 13 :
Total Pages : 170 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis High Reynolds Number Tests of a NASA SC(3)-0712(B) Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel by : William Garland Johnson

Download or read book High Reynolds Number Tests of a NASA SC(3)-0712(B) Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel written by William Garland Johnson and published by . This book was released on 1985 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind Tunnel Test Techniques

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Publisher : Academic Press
ISBN 13 : 0128181001
Total Pages : 672 pages
Book Rating : 4.1/5 (281 download)

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Book Synopsis Wind Tunnel Test Techniques by : Colin Britcher

Download or read book Wind Tunnel Test Techniques written by Colin Britcher and published by Academic Press. This book was released on 2023-10-20 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind Tunnel Test Techniques: Design and Use at Low and High Speeds with Statistical Engineering Applications provides an up-to-date treatment of the topic. Beginning with a brief history of wind tunnels and its types and uses, the book goes on to cover subsonic, supersonic and hypersonic wind tunnel design and construction, calibration, boundary corrections, flow quality assessment, pressure surveys, and dynamic testing. It also focuses on wind tunnel facilities, making it useful for both the designer and operator. Engineers and graduate students in aerospace, automotive and similar programs will find this book useful in their work with experimental aerodynamics, gas dynamics, facility design and performance. Deals with a broad range of flow speeds in wind tunnels, from low speed to high speed Provides a discussion of similarity laws as well as material on statistical analysis Includes coverage on facility-to-facility and facility-to-CFD correlation Presents advanced topics such as cryogenic wind tunnels, ground simulation in automotive testing, and propulsion testing

Flow-visualization Techniques Used at High Speed by Configuration Aerodynamics Wind-tunnel-test Team

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Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Flow-visualization Techniques Used at High Speed by Configuration Aerodynamics Wind-tunnel-test Team by : John E. Lamar

Download or read book Flow-visualization Techniques Used at High Speed by Configuration Aerodynamics Wind-tunnel-test Team written by John E. Lamar and published by . This book was released on 2001 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper summarizes a variety of optically based flow-visualization techniques used for high-speed research by the Configuration Aerodynamics Wind-Tunnel-Test Team of the High-Speed Research Program during its tenure. The work of other national experts is included for completeness. Details of each technique with applications and status in various national wind tunnels are given.

Scale Effects on Aircraft and Weapon Aerodynamics

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ISBN 13 :
Total Pages : 258 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scale Effects on Aircraft and Weapon Aerodynamics by : A. B. Haines

Download or read book Scale Effects on Aircraft and Weapon Aerodynamics written by A. B. Haines and published by . This book was released on 1994 with total page 258 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Reynolds Number Effects in Transonic Flow

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ISBN 13 : 9789283504924
Total Pages : 82 pages
Book Rating : 4.5/5 (49 download)

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Book Synopsis Reynolds Number Effects in Transonic Flow by : A. Elsenaar

Download or read book Reynolds Number Effects in Transonic Flow written by A. Elsenaar and published by . This book was released on 1988 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: Reynolds number effects in transonic flow are critically reviewed. This review, which may be considered a supplement to AR 224 'Boundary Layer Simulation and Control in Wind Tunnels', is mainly concered with a discussion of viscous effects actually observed on realistic configurations. The following geometries are considered: Airfoils and high aspect ratio wings typical and transport aircraft, fighter-type low aspect ratio delta wings, tow- and three-dimensional bodies characteristic of missiles and combat aircraft fuselages, and afterbodies. "Pseudo"--Reynolds number on the wind tunnel environment and in turn affect the flow about a model. As an introduction, a brief retrospect of the "history" of Reynolds number effect is presented. This AGARDograph has been produced at the request of the Fluid Dynamics Panel of AGARD.

Measurements of Fluctuating Pressure in a Rectangular Cavity in Transonic Flow at High Reynolds Numbers

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Measurements of Fluctuating Pressure in a Rectangular Cavity in Transonic Flow at High Reynolds Numbers by : M. B. Tracy

Download or read book Measurements of Fluctuating Pressure in a Rectangular Cavity in Transonic Flow at High Reynolds Numbers written by M. B. Tracy and published by . This book was released on 1992 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Measurements of Fluctuating Pressure in a Rectangular Cavity in Transonic Flow at High Reynolds Numbers

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Measurements of Fluctuating Pressure in a Rectangular Cavity in Transonic Flow at High Reynolds Numbers by : M. B. Tracy

Download or read book Measurements of Fluctuating Pressure in a Rectangular Cavity in Transonic Flow at High Reynolds Numbers written by M. B. Tracy and published by . This book was released on 1992 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Cryogenic Wind-tunnel Concept for High Reynolds Number Testing

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Publisher :
ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis The Cryogenic Wind-tunnel Concept for High Reynolds Number Testing by :

Download or read book The Cryogenic Wind-tunnel Concept for High Reynolds Number Testing written by and published by . This book was released on 1974 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

High Speed Wind Tunnel Testing

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Publisher : John Wiley & Sons
ISBN 13 :
Total Pages : 496 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis High Speed Wind Tunnel Testing by : Alan Pope

Download or read book High Speed Wind Tunnel Testing written by Alan Pope and published by John Wiley & Sons. This book was released on 1965-01-15 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt: