Download or read book Hypersonic Shock Tunnel written by Cornell Aeronautical Laboratory. Experimental Facilities Division and published by . This book was released on 1964 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book 48 inch Hypersonic Shock Tunnel written by Cornell Aeronautical Laboratory and published by . This book was released on 1962 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Hypersonic Shock Tunnel written by Raghuram Gopalrao Murtugudde and published by . This book was released on 1986 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low density Research in the Hypersonic Shock Tunnel written by Charles E. Wittliff and published by . This book was released on 1960 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Shock Waves Marseille I written by Raymond Brun and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 497 pages. Available in PDF, EPUB and Kindle. Book excerpt: Recently, there have been significant advances in the fields of high-enthalpy hypersonic flows, high-temperature gas physics, and chemistry shock propagation in various media, industrial and medical applications of shock waves, and shock-tube technology. This series contains all the papers and lectures of the 19th International Symposium on Shock Waves held in Marseille in 1993. They are published in four topical volumes, each containing papers on related topics, and preceded by an overview written by a leading international expert. The volumes may be purchased independently.

Download or read book Hypersonic Research in the Shock Tunnel written by Charles E. Wittliff and published by . This book was released on 1960 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flow Phenomena in Starting a Hypersonic Shock Tunnel written by Herbert S. Glick and published by . This book was released on 1955 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Hypersonic Shock Tunnel written by Calspan Corporation and published by . This book was released on 1987 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book THE AEROSPACE HYPERSONIC SHOCK TUNNEL written by and published by . This book was released on 1963 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Aerospace Hypersonic Shock Tunnel is described along with an initial calibration at flow Mach numbers of 12, 14, 17, and 18. Room temperature helium is used as the driver gas. Efforts to drive the shock tunnel with com bustion heated helium have been made, and these experiments are also described.

Download or read book Advanced Hypersonic Test Facilities written by Frank K. Lu and published by AIAA. This book was released on 2002 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Design of a Hypersonic Shock Tunnel written by Derrill Gene Whitten and published by . This book was released on 1958 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Theories and Technologies of Hypervelocity Shock Tunnels written by Zonglin Jiang and published by Cambridge University Press. This book was released on 2023-10-26 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt: Introducing the state-of-the-art of hypervelocity shock tunnels, this complete reference features a variety of drivers and step-by-step introductions to their theories, physics, methods and testing. This book enables researchers and engineers in aerospace to design and improve wind tunnels that simulate flow qualities of real hypersonic flyers.

Download or read book The Convair Free Jet Hypersonic Shock Tunnel Part I the State of the Working Gas Entering the Test Section Part Ii Hypersonic Shock Tunnel Jet Analysis ideal Gas written by KARL A. FAYMON and published by . This book was released on 1959 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: The thermodynamic, electronic, and chemical state of the working gas of a shock tube as it enters the test or working section is investigated. Included are real gas effects and an evaluation of the effect of the bursting diaphragm on the gas state. The bursting diaphragm was found to have negligible effect on the state of the working gas entering the shock tube test section. The results are presented in graphical form showing the states which would exist at the test section entrance as a function of the driverdriven gas diaphragm pressure ratios when the driver gas is a mixture of Helium-OxygenHydrogen. (Author).

Download or read book A THEORETICAL ANALYSIS OF THE DRIVERRESERVOIR METHOD OF DRIVING HYPERSONIC SHOCK TUNNELS written by Canada. Defence Research Board and published by . This book was released on 1964 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt: The driver-reservoir method of extending the test time of a tailored hypersonic shock tunnel by using a reservoir and a nozzle (perforated plate) at the upstream end of the driver is treated theoretically. It is shown that the flow following the rupture of the diaphragm is highly complex and contains both steady and unsteady flow regimes. It is also shown that the area ratio of the nozzle separating the driver from the reservoir determines the nature of the wave system produced. For a unique or 'ideal' nozzle area ratio a flow system is produced which contains no downstream running disturbances other than Mach waves. That is, both the head and the tail of the initial rarefaction wave are prevented from interfering with the shock-tunnel reservoir. Consequently, the running time of the shock tunnel can be extended. The ideal area ratios are calculated for a wide range of shock tunnel operating conditions and compared with experimental results. The comparison shows that the ideal nozzle area ratio can be predicted accurately from theory. (Author).

Download or read book Hypersonic Shock Tunnel written by Henry T. Nagamatsu and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Hypersonic Shock Tunnel Performance Characteristics written by Douglas Hutton May (CAPT, USAF.) and published by . This book was released on 1974 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Performance of a Hypersonic Shock Tunnel Incorporating a Monotonic Area Reduction at the Diaphragm of the Shock Tube written by John Benjamin Hinkey and published by . This book was released on 1990 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt: