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 The Design of a Hypersonic Shock Tunnel written by Robert D. Stewart and published by . This book was released on 1957 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Design of a Mach Number Eight Hypersonic Shock Tunnel written by Pildong Chey and published by . This book was released on 1970 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Initial Instrumentation Design for the University of Washington Hypersonic Shock Tunnel written by Errol Wayne Robinson and published by . This book was released on 1958 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Design and Construction of a Hypersonic Shock Tunnel written by Nasim Farrukh Amin and published by . This book was released on 1964 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt: "A combustion driven hypersonic shock tunnel has been designed and constructed primarily for the simulation of flows around hypersonic ramjets. This report describes the design and construction of the shock tunnel and discusses its hypersonic simulation capabilities. The construction of the shock tunnel has now been completed and it is ready for instrumentation and calibration. The driving gas is a combustible mixture of stoichiometric hydrogen and oxygen diluted with 60 to 75% helium to avoid detonation. The maximum mixture loading pressure is 2000 psi. The driven gas is air, usually at room temperature and pressure. Successful evacuation of the test section to 5 microns of mercury has been achieved. The shock tunnel has been designed to produce air at minimum stagnation temperature and pressure of 4200°R and 2300 psi respectively and 0 maximum stagnation temperature and pressure of 14300°R and 20,000 psi respectively1 at the nozzle entrance. Air at these stagnation conditions, when expanded in the test section, will completely simulate free flight conditions (i.e., pressure, temperature, unit Reynold's number, Mach number, etc.) in and around a hypersonic ramjet flying over an altitude range of 90,000 ft to 250,000 ft and a corresponding Mach number range of 7.5 to 18.5. Preliminary tests have been successful and have indicated that (a) the recoil mechanism is capable of absorbing the shock forces, (b) the gun barrels, joined end to end, produce a well aligned, rigid and strong driven section and (c) the actual recoil stroke will probably be considerably less than the initially assumed value of 4"." --
Download or read book Design and Characteristics of a Small Hypersonic Shock Tunnel Combustion Driver written by R. E. Duffy and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: A combustion driver for a small Hypersonic Shock Tunnel has been designed and tested. Combustion pressure-time histories for stoichiometric hydrogen and oxygen mixtures diluted with varying percentages of helium have been obtained. Tests indicate that the combustion results are repeatable and peak combustion pressure and temperature are controllable within a wide range. The dimensions of combustion drivers appear to have an important effect in that rough burning conditions, reported by other investigators, have not been noticeable except at very low percentage concentrations of helium.
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 The Design Development and Calibration of a Tailored Interface Hypersonic Shock Tunnel for Supersonic Combustion Research written by Michael Peter Wood and published by . This book was released on 1968 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book On the Design and Testing of a Mach 6 Nozzle for a Shock Reflect Type Hypersonic Shock Tunnel written by F. M. Yu and published by . This book was released on 1994 with total page 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 Design Features of the General Electric Research Laboratory Hypersonic Shock Tunnel written by Henry T. Nagamatsu and published by . This book was released on 1961 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design features of the General Electric Research Laboratory hypersonic shock tunnel are described. Particular emphasis is placed on many of its unique features. The loading and ignition system for consistent driver combustion without detonation is discussed. The anchoring of the driver and the slip joint clamping section that holds the main scored diaphragm is described in some detail. By boring and honing the stainless steel tubes, the attenuation of the shock wave in the long driven section was minimized. The use of a second diaphragm and a slip joint at the entrance to a conical nozzle is explained. The development of instrumentation necessary for shock tunnel operation is shown to have progressed to a point where the hypersonic shock tunnel is an extremely useful and versatile tool for hypersonic research. It is possible to simulate the Mach numbers and temperatures encountered by ICBM's, satellites, and space vehicles at the high altitude conditions. (Author).
Download or read book Design Construction and Performance of a Hypersonic Shock Tube written by Jack Goodman and published by . This book was released on 1969 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Design Fabrication and Calibration of a Mach 6 5 Hypersonic Shock Tunnel Nozzle for Scramjet Testing Applications written by Dean Modroukas and published by . This book was released on 1998 with total page 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 315 pages. Available in PDF, EPUB and Kindle. Book excerpt: A comprehensive reference on the basics, physics, design methods, and testing of various state-of-the art hypervelocity shock tunnels.
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 Design of a Supersonic Shock Tunnel and Experimental Surface Measurements written by Yagnavalkya S. Mukkamala and published by . This book was released on 1993 with total page 216 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Combustion Driven Shock Tunnel of the Polytechnic Institute of Brooklyn written by Marian Visich (Jr) and published by . This book was released on 1965 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt: A hypersonic shock tunnel has been designed and constructed for obtaining fluid dynamic and electromagnetic properties of the flow field around hypersonic reentry bodies. In this report the design philosophy and a description of the combustion driven shock tunnel of the Polytechnic Institute of Brooklyn is presented as well as the estimated performance of the shock tunnel over a range of test section stagnation conditions. (Author).
