Download or read book The Kinetics and Effects of Air Condensation in the A R L Hypersonic Wind Tunnel written by A. S. Kaye and published by . This book was released on 1972 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Air Condensation Effects Measured in the RAE 7 In X 7 In Hypersonic Wind Tunnel written by J.F.W. Crane and published by . This book was released on 1966 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1973 with total page 1102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NOL Mach 18 Hypervelocity Research Tunnel written by Ray H. Cornett and published by . This book was released on 1974 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic capabilities and physical characteristics of the Naval Ordnance Laboratory's Mach number 18 Hypervelocity Research Tunnel are described. This tunnel is a high-pressure, blowdown-type facility that uses nitrogen as the working gas. The facility provides a maximum test section Reynolds number of 0.2 million per meter (0.7 million per foot) at the maximum stagnation pressure of 700 atmospheres and a supply temperature of 2100 Kelvin. A forced-convection electric heater with a graphite heater element is used to achieve the required flow temperatures. The axisymmetric, contoured nozzle is 3.96 meters long with an exit diameter of 0.61 meters. Flow times are from one to four minutes.

Download or read book Theoretical and Experimental Investigation of Condensation of Air in Hypersonic Wind Tunnels written by H. Guyford Stever and published by . This book was released on 1951 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of theoretical and experimental investigations of condensation of air in hypersonic wind tunnels. The experimental work was done in a tunnel with Mach number of approximately 7. Condensation was detected and measured by condensation-fog, light-scattering, static-pressure measurements, and changes in wedge shock angle at degrees of supersaturation considerably lower than those predicted by existing condensation theory. Effects of varying supply pressures and temperatures were also measured. The nucleation theory of condensation was modified to take account of a postulated variation of surface tension with decrease in size of spontaneously formed drops which act as nuclei of condensation. The modified theory was applied to pure oxygen and nitrogen and its predictions were compared with those of the unmodified theory.

Download or read book STAR written by and published by . This book was released on 1966 with total page 1204 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Air Force Research Resum s written by and published by . This book was released on with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Report written by Aeronautical Research Laboratories (Australia) and published by . This book was released on 1971 with total page 382 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Chemical Kinetic Regimes of Hypersonic Flight Simulation written by Donald J. Harney and published by . This book was released on 1963 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Condensation of Air in Supersonic Wind Tunnels and Its Effects on Flow about Models written by C. Frederick Hansen and published by . This book was released on 1952 with total page 49 pages. Available in PDF, EPUB and Kindle. Book excerpt: Condensation of air in supersonic wind tunnels is investigated. Theoretical limits of the threshold of condensation are calculated and compared with experiment. Test results are presented which indicate the effectiveness of water vapork, carbon dioxide, and silica gel as condensation nuclei in supersaturated air. The properties of a partially condensed supersonic air stream are estimated and the effects of condensation phenomena in flow about models are examined.

Download or read book OAR Cumulative Index of Research Results written by United States. Air Force. Office of Aerospace Research and published by . This book was released on 1965 with total page 586 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Condensation of air components in hypersonic wind tunnels written by Rolf D. Buhler and published by . This book was released on 1952 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Aeronautical Journal written by and published by . This book was released on 1973 with total page 426 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book U S Government Research Reports written by and published by . This book was released on 1963 with total page 350 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book OAR Cumulative Index of Research Results written by and published by . This book was released on with total page 788 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Condensation in Hypersonic Wind Tunnels written by Jack Werner and published by . This book was released on 1949 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The High Temperature Aspects of Hypersonic Flow written by Wilbur C. Nelson and published by Elsevier. This book was released on 2014-12-02 with total page 801 pages. Available in PDF, EPUB and Kindle. Book excerpt: The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.