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EBookClubs

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Book Wind Tunnel Test Techniques

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

Book Design  Construction and Calibration of a Small Subsonic Wind Tunnel

Download or read book Design Construction and Calibration of a Small Subsonic Wind Tunnel written by William Lee Lewis and published by . This book was released on 1970 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Part 1  Construction and Calibration of the McGill Supersonic Wind Tunnel

Download or read book Part 1 Construction and Calibration of the McGill Supersonic Wind Tunnel written by Chi. K. Kwok and published by . This book was released on 1962 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: "The design and construction of the McGill intermittent, suckdown supersonic wind tunnel and its instrumentations are described. It operates on the pressure differential between the atmosphere and a 320 cu. ft. vacuum. storage tank. The running time for Mach number of 1 .8 is in the vicinity of twelve seconds with a test section area of approximately four sq. in.. Theoretical as well as experimental performance curves for the wind tunnel are presented. Calibrations of a Mach 1.8 axisymmetric nozzle and a Mach 1.8 two-dimensional nozzle are given in detail. The Mach number distribution compares favourably with other supersonic wind tunnels. The tunnel is being used to study supersonic flow in ducts, and problems concerning multiple shock waves and orifice experiments." --

Book The Design  Construction and Calibration of a Small Wind Tunnel

Download or read book The Design Construction and Calibration of a Small Wind Tunnel written by Roy Valentine Smith and published by . This book was released on 1950 with total page 460 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Design and Construction of a Calibration Wind Tunnel

Download or read book The Design and Construction of a Calibration Wind Tunnel written by Carl F. Shreder and published by . This book was released on 1988 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Design  Construction and Calibration of the M I T  4 1 2 by 6 Foot Student Wind Tunnel

Download or read book Design Construction and Calibration of the M I T 4 1 2 by 6 Foot Student Wind Tunnel written by Lawrence Bernbaum and published by . This book was released on 1948 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Diffuser Efficiency and Flow Process of Supersonic Wind Tunnels with Free Jet Test Section

Download or read book Diffuser Efficiency and Flow Process of Supersonic Wind Tunnels with Free Jet Test Section written by Rudolf Hermann and published by . This book was released on 1950 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the wind tunnel arrangement under consideration, the air leaves the Laval nozzle as a free jet and is recaptured by the diffuser, which is of the convergent-divergent design. A theoretical analysis of the flow process through this type of supersonic wind tunnel is presented and the diffuser efficiency is calculated for the case of equilibrium between test chamber pressure and pressure in the nozzle exit, assuming one-dimensional, in viscous, steady flow. Using the basic equations of continuity, energy and momentum flux through a bounding surface, an exact solution of the problem is obtained, which is applicable up to Mach number infinite. One of the basic results is, that in the recapturing zone of the diffuser a transition occurs from supersonic to subsonic flow, which is followed by an acceleration in the convergent portion up to sonic velocity at the second throat. The transition is not a normal shock and involves a total pressure loss greater than that of a normal shock at the test section Mach number. A mathematical solution with supersonic velocity after the transition process has no physical existence. A comprehensive comparison of the analytical results with available experiments in supersonic wind tunnels up to Mach number 4.4 regarding diffuser efficiency and second throat area shows good agreement.

Book The Design  Construction  and Proof of a Supersonic Wind Tunnel

Download or read book The Design Construction and Proof of a Supersonic Wind Tunnel written by Wendell Davis and published by . This book was released on 1951 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Design and Construction of a Supersonic Wind Tunnel

Download or read book Design and Construction of a Supersonic Wind Tunnel written by Lawrence Fred Smith and published by . This book was released on 1956 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Design  Construction  and Calibration of a Boundary layer Research Wind Tunnel

Download or read book Design Construction and Calibration of a Boundary layer Research Wind Tunnel written by Omeed Alahverdizadeh and published by . This book was released on 1985 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt: