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Author : WALTER P. REHM
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)
Download or read book Supersonic Wind Tunnel Tests on Experimental Static Pressure Probes written by WALTER P. REHM and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Harry Edward Bailey
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (798 download)
Download or read book An Experimental Evaluation of a Wedge-type Free-stream Static-pressure Probe written by Harry Edward Bailey and published by . This book was released on 1952 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Rudolf Hermann
Publisher :
ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.:/5 (2 download)
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.
Author :
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)
Download or read book Experimental Investigation of the Subsonic High-altitude Operation of the NASA Lewis 10- by 10-foot Supersonic Wind Tunnel written by and published by . This book was released on 1988 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : J. L. Lindsey
Publisher :
ISBN 13 :
Total Pages : 53 pages
Book Rating : 4.:/5 (227 download)
Download or read book Interference Effects Due to Relative Proximity of Static-pressure Probes in Supersonic Flow written by J. L. Lindsey and published by . This book was released on 1957 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in a supersonic wind tunnel to determine the minimum critical spacing for no mutual interference of two cone-cylinder-type static-pressure probes designed for simultaneous pressure measurement in supersonic flow. Tests made over a Mach Number range of approximately 1.9 through 3.4 indicate that the minimum critical spacing is predominately a function of Mach Number and static-orifice location. Probe cone-angle and probe diameter variations produce minor effects. A theoretical study of static-orifice location was also made. Results indicate that the generally recommended position of six to ten probe diameters aft of the cone shoulder is suitable for pressure measurement at Mach Numbers as high as approximately 3.5; however, higher velocities require static-orifice locations at greater distances from the cone shoulder. (Author).
Author : P. E. Culbertson
Publisher :
ISBN 13 :
Total Pages : 47 pages
Book Rating : 4.3/5 (91 download)
Download or read book Calibration Report on the University of Michigan Supersonic Wind Tunnel written by P. E. Culbertson and published by . This book was released on 1949 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jorge Colman Lerner
Publisher : BoD – Books on Demand
ISBN 13 : 9533076232
Total Pages : 728 pages
Book Rating : 4.5/5 (33 download)
Download or read book Wind Tunnels and Experimental Fluid Dynamics Research written by Jorge Colman Lerner and published by BoD – Books on Demand. This book was released on 2011-07-27 with total page 728 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book "Wind Tunnels and Experimental Fluid Dynamics Research" is comprised of 33 chapters divided in five sections. The first 12 chapters discuss wind tunnel facilities and experiments in incompressible flow, while the next seven chapters deal with building dynamics, flow control and fluid mechanics. Third section of the book is dedicated to chapters discussing aerodynamic field measurements and real full scale analysis (chapters 20-22). Chapters in the last two sections deal with turbulent structure analysis (chapters 23-25) and wind tunnels in compressible flow (chapters 26-33). Contributions from a large number of international experts make this publication a highly valuable resource in wind tunnels and fluid dynamics field of research.
Author : Alan Pope
Publisher : John Wiley & Sons
ISBN 13 :
Total Pages : 496 pages
Book Rating : 4.3/5 (91 download)
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 : Ethirajan Rathakrishnan
Publisher : CRC Press
ISBN 13 : 1315394855
Total Pages : 613 pages
Book Rating : 4.3/5 (153 download)
Download or read book Instrumentation, Measurements, and Experiments in Fluids written by Ethirajan Rathakrishnan and published by CRC Press. This book was released on 2016-12-19 with total page 613 pages. Available in PDF, EPUB and Kindle. Book excerpt: Mechanical engineers involved with flow mechanics have long needed an authoritative reference that delves into all the essentials required for experimentation in fluids, a resource that can provide fundamental review, as well as the details necessary for experimentation on everything from household appliances to hi-tech rockets. Instrumentation, Measurements, and Experiments in Fluids meets this challenge, as its author is not only a highly respected pioneer in fluids, but also possesses twenty years experience teaching students of all levels. He clearly explains fundamental principles as well the tools and methods essential for advanced experimentation. Reflecting an awe for flow mechanics, along with a deep-rooted knowledge, the author has assembled a fourteen chapter volume that is destined to become a seminal work in the field. Providing ample detail for self study and the sort of elegant writing rarely found in so thorough a treatment, he provides insight into all the vital topics and issues associated with the devices and instruments used for fluid mechanics and gas dynamics experiments. Extremely organized, this work presents easy access to the principles behind the science and goes on to elucidate the current research and findings needed by those seeking to make further advancement. Unique and Thorough Coverage of Uncertainty Analysis The author provides valuable insight into the vital issues associated with the devices used in fluid mechanics and gas dynamics experiments. Leaving nothing to doubt, he tackles the most difficult concepts and ends the book with an introduction to uncertainty analysis. Structured and detailed enough for self study, this volume also provides the backbone for both undergraduate and graduate courses on fluids experimentation.
Author : Jerry M. Allen
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Pitot-probe Displacement in a Supersonic Turbulent Boundary Layer written by Jerry M. Allen and published by . This book was released on 1972 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Eight circular pitot probes ranging in size from 2 to 70 percent of the boundary-layer thickness were tested to provide experimental probe displacement results in a two-dimensional turbulent boundary layer at a nominal free-stream Mach number of 2 and unit Reynolds number of 8 million per meter. The displacement obtained in the study was larger than that reported by previous investigators in either an incompressible turbulent boundary layer or a supersonic laminar boundary layer. The large probes indicated distorted Mach number profiles, probably due to separation. When the probes were small enough to cause no appreciable distortion, the displacement was constant over most of the boundary layer. The displacement in the near-wall region decreased to negative displacement in some cases. This near-wall region was found to extend to about one probe diameter from the test surface.
Author : Ethirajan Rathakrishnan
Publisher : CRC Press
ISBN 13 : 1351848577
Total Pages : 613 pages
Book Rating : 4.3/5 (518 download)
Download or read book Instrumentation, Measurements, and Experiments in Fluids, Second Edition written by Ethirajan Rathakrishnan and published by CRC Press. This book was released on 2020-02-06 with total page 613 pages. Available in PDF, EPUB and Kindle. Book excerpt: Instrumentation, Measurements, and Experiments in Fluids, Second Edition is primarily focused on essentials required for experimentation in fluids, explaining basic principles, and addressing the tools and methods needed for advanced experimentation. It also provides insight into the vital topics and issues associated with the devices and instruments used for fluid mechanics and gas dynamics experiments. The second edition adds exercise problems with answers, along with PIV systems of flow visualization, water flow channel for flow visualization, and pictures with Schlieren and shadowgraph—from which possible quantitative information can be extracted. Ancillary materials include detailed solutions manual and lecture slides for the instructors.
Author :
Publisher :
ISBN 13 :
Total Pages : 464 pages
Book Rating : 4.:/5 (3 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 464 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jerome Clarke Hunsaker
Publisher :
ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.3/5 (91 download)
Download or read book Reports on Wind Tunnel Experiments in Aerodynamics written by Jerome Clarke Hunsaker and published by . This book was released on 1916 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : CALIBRATION REPORT ON THE UNIVERSITY OF MICHIGAN SUPERSONIC WIND TUNNEL
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.L/5 ( download)
Download or read book P. E. CULBERTSON written by CALIBRATION REPORT ON THE UNIVERSITY OF MICHIGAN SUPERSONIC WIND TUNNEL and published by . This book was released on 1952 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 154 pages
Book Rating : 4.:/5 (317 download)
Download or read book Baseline Calibration of the NASA Lewis Research Center 8-by 6-Foot Supersonic Wind Tunnel (1991 and 1992 Tests) written by and published by . This book was released on 1998 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Samuil Matusovich Gorlin
Publisher :
ISBN 13 :
Total Pages : 612 pages
Book Rating : 4.X/5 ( download)
Download or read book Wind Tunnels and Their Instrumentation written by Samuil Matusovich Gorlin and published by . This book was released on 1966 with total page 612 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)
Download or read book Flow Field Surveys of the NASA Lewis Research Center 8- by 6-Foot Supersonic Wind Tunnel (1993 Test) written by and published by . This book was released on 1998 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
