Transonic Wind Tunnel Testing PDF Download
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Author | : B. H. Goethert |
Publisher | : |
Total Pages | : 420 |
Release | : 2007 |
Genre | : Science |
ISBN | : |
Download Transonic Wind Tunnel Testing Book in PDF, ePub and Kindle
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 | : |
Total Pages | : |
Release | : 1985 |
Genre | : Transonic wind tunnels |
ISBN | : |
Download Transonic Wind Tunnel Testing Book in PDF, ePub and Kindle
Author | : Bernard H. Goethert |
Publisher | : |
Total Pages | : |
Release | : 1961 |
Genre | : Transonic wind tunnels |
ISBN | : |
Download Transonic Wind Tunnel Testing Book in PDF, ePub and Kindle
Author | : Alan Pope |
Publisher | : |
Total Pages | : 0 |
Release | : 1978 |
Genre | : |
ISBN | : |
Download High-speed Wind Tunnel Testing Book in PDF, ePub and Kindle
Author | : Colin Britcher |
Publisher | : Academic Press |
Total Pages | : 672 |
Release | : 2023-10-20 |
Genre | : Technology & Engineering |
ISBN | : 0128181001 |
Download Wind Tunnel Test Techniques Book in PDF, ePub and Kindle
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 |
Total Pages | : 496 |
Release | : 1965-01-15 |
Genre | : Science |
ISBN | : |
Download High Speed Wind Tunnel Testing Book in PDF, ePub and Kindle
Author | : Luigi Crocco |
Publisher | : |
Total Pages | : 230 |
Release | : 1946 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download High-speed Wind Tunnels Book in PDF, ePub and Kindle
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 | : Francis J. Capone |
Publisher | : |
Total Pages | : 20 |
Release | : 1961 |
Genre | : Transonic wind tunnels |
ISBN | : |
Download Transonic Wind-tunnel Tests of an Error-compensated Static-pressure Probe Book in PDF, ePub and Kindle
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 | : A. M. Whitnah |
Publisher | : |
Total Pages | : 524 |
Release | : 1984 |
Genre | : |
ISBN | : |
Download Space shuttle wind tunnel testing program summary Book in PDF, ePub and Kindle
Author | : William C. Moseley (Jr.) |
Publisher | : |
Total Pages | : 84 |
Release | : 1966 |
Genre | : Aerospace engineering |
ISBN | : |
Download Apollo Wind Tunnel Testing Program Book in PDF, ePub and Kindle