Transonic Wind Tunnel Testing

Author : B. H. Goethert
Publisher :
ISBN 13 :
Total Pages : 420 pages
Book Rating : 4.13/5 ( download)

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Download or read book Transonic Wind Tunnel Testing written by B. H. Goethert and published by . This book was released on 2007 with total page 420 pages. Available in PDF, EPUB and Kindle. Book excerpt: Numerous aspects of transonic aerodynamics include wall interference corrections in conventional wind tunnels, subsonic flow in a variety of wind tunnels, and test results from transonic wind tunnels. 1961 edition.

Author : Bernhard H. Goethert
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.56/5 ( download)

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Download or read book Transonic Wind Tunnel Testing written by Bernhard H. Goethert and published by . This book was released on 1985 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Bernard H. Goethert
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.02/5 ( download)

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Download or read book Transonic Wind Tunnel Testing written by Bernard H. Goethert and published by . This book was released on 1961 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Alan Pope
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.96/5 ( download)

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Download or read book High-speed Wind Tunnel Testing written by Alan Pope and published by . This book was released on 1978 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Colin Britcher
Publisher : Academic Press
ISBN 13 : 0128181001
Total Pages : 672 pages
Book Rating : 4.03/5 ( download)

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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

Author : Alan Pope
Publisher : John Wiley & Sons
ISBN 13 :
Total Pages : 496 pages
Book Rating : 4.47/5 ( download)

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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:

Author : Francis J. Capone
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.33/5 ( download)

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Download or read book Transonic Wind-tunnel Tests of an Error-compensated Static-pressure Probe written by Francis J. Capone and published by . This book was released on 1961 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the pressure-sensing characteristics of an error-compensated static-pressure probe mounted on the nose section of a missile body has been conducted in the Langley 16-foot transonic tunnel. The probe was free to rotate about its roll axis and was equipped with a vane so that the crossflow velocity component due to angles of attack of sideslip was always alined with the probe's vertical plane of symmetry. The probe was tested in five axial positions with respect to the missile nose at Mach numbers from 0.30 to 1.08 and at angles of attack from -2.7° to 15.3°. The test Reynolds number per foot varied from 1.79 x 106 to 4.05 x 106. Results showed that at a Mach number of 1.00 the static-pressure error decreased from 3.5 percent to 0.8 percent of the free-stream static pressure, as a result of a change in orifice location from 0.15 maximum missile diameter to 0.20 maximum missile diameter forward of the missile nose. Although compensation for pressure-sensing errors due to angles of attack up to 15.3 was maintained at Mach numbers from M = 0.30 to M = 0.50, there was an increase in error with an increase in angle of attack for Mach numbers between M = 0.50 and M = 1.08.

Author : Luigi Crocco
Publisher :
ISBN 13 :
Total Pages : 230 pages
Book Rating : 4.73/5 ( download)

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Download or read book High-speed Wind Tunnels written by Luigi Crocco and published by . This book was released on 1946 with total page 230 pages. Available in PDF, EPUB and Kindle. Book excerpt: The importance assumed in recent times by experimental supersonic wind tunnels, as well as the power required, has brought about the need for a study which would permit a comparison of the types tested and the principal theoretical plans.

Author : A. M. Whitnah
Publisher :
ISBN 13 :
Total Pages : 524 pages
Book Rating : 4.79/5 ( download)

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Download or read book Space shuttle wind tunnel testing program summary written by A. M. Whitnah and published by . This book was released on 1984 with total page 524 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : William C. Moseley (Jr.)
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.31/5 ( download)

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Download or read book Apollo Wind Tunnel Testing Program written by William C. Moseley (Jr.) and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: