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The Design Instrumentation And Operation Of The Utia Low Density Wind Tunnel
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Book Synopsis Design and Calibration of an Arc-heated, Hypersonic, Low-density Wind Tunnel by : Ruth N. Weitmann
Download or read book Design and Calibration of an Arc-heated, Hypersonic, Low-density Wind Tunnel written by Ruth N. Weitmann and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Report written by and published by . This book was released on 1964 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1969 with total page 468 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis UTIA Technical Note by : University of Toronto. Institute of Aerophysics
Download or read book UTIA Technical Note written by University of Toronto. Institute of Aerophysics and published by . This book was released on 1962 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis AFOSR. by : United States. Air Force. Office of Scientific Research
Download or read book AFOSR. written by United States. Air Force. Office of Scientific Research and published by . This book was released on 1957 with total page 1136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Characteristics of a Continuous-flow Induction Plasma Accelerator by : J. D. Brooks
Download or read book Characteristics of a Continuous-flow Induction Plasma Accelerator written by J. D. Brooks and published by . This book was released on 1965 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Characteristics of continuous-flow induction plasma accelerators with a 10-kilocycle, single-phase driving coil on supersonic nozzles were studied. Pressure measurements and vane-deflection measurements were made in a 15-centimeter-diameter accelerator at various mass flow rates. Charged-particle velocities were obtained in 15-centimeter-diameter and 10-centimeter-diameter accelerators by measuring with photoelectric detectors the time required for a change in flow luminosity to travel a known distance. Pressure-probe measurements indicated that the entire flow, including the boundary layer and the separated-flow region, was accelerated in the 15-centimeter-diameter accelerator. The largest increase in pilot pressure was 250 percent of the cold-flow value with 20 kilowatts of 10-kilocycle driving power. The charged-particle velocities increased as the mass flow rate was reduced and as the power was increased. The maximum charged-particle velocity obtained was 40,000 meters per second in the 10-centimeter-diameter accelerator. Average velocity and thrust obtained from vane-deflection measurements were in good agreement with those obtained from pressure-probe measurements.
Download or read book UTIAS Report written by and published by . This book was released on 1959 with total page 470 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1977 with total page 1072 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Progress Report on Research Supported by Grants from the Defense Research Board of Canada by : University of Toronto. Institute for Aerospace Studies
Download or read book Progress Report on Research Supported by Grants from the Defense Research Board of Canada written by University of Toronto. Institute for Aerospace Studies and published by . This book was released on 1990 with total page 378 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1948 with total page 770 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of a Plasma Accelerator with Magnetic Field Arranged to Produce a Divergent-nozzle Effect by : Joseph D. Brooks
Download or read book Investigation of a Plasma Accelerator with Magnetic Field Arranged to Produce a Divergent-nozzle Effect written by Joseph D. Brooks and published by . This book was released on 1969 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design and Operation of a Continuous-flow Hypersonic Wind Tunnel Using a Two-dimensional Nozzle by : Harris M. Schurmeier
Download or read book Design and Operation of a Continuous-flow Hypersonic Wind Tunnel Using a Two-dimensional Nozzle written by Harris M. Schurmeier and published by . This book was released on 1959 with total page 306 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Air Force Scientific Research Bibliography by : Library of Congress. Science and Technology Division
Download or read book Air Force Scientific Research Bibliography written by Library of Congress. Science and Technology Division and published by . This book was released on 1964 with total page 1136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis UTIA Review by : University of Toronto. Institute of Aerophysics
Download or read book UTIA Review written by University of Toronto. Institute of Aerophysics and published by . This book was released on 1961 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Behaviour of Free Molecule Cylindrical Langmuir Probes in Supersonic Flows, and Their Application to the Study of the Blunt Body Stagnation Layer by : A. A. Sonin
Download or read book The Behaviour of Free Molecule Cylindrical Langmuir Probes in Supersonic Flows, and Their Application to the Study of the Blunt Body Stagnation Layer written by A. A. Sonin and published by . This book was released on 1965 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experiments were performed in an RF generated, low density plasma flow to determine the behaviour of small, cylindrical Langmuir probes in high-speed flows. All mean free paths were large compared to the probe diameter except the mean free path for ion-ion collisions. The tests indicated that under simulated static conditions (probe axis parallel to flow velocity), the theory of Laframboise represented the ion current characteristic well when the ratio between radius of probe and Debye length was large, but not when the probe radius was comparable to or smaller than the Debye length. The results indicated clearly that the ion current decreased with increasing normal velocity, reached a minimum, and then increased again for subsequent increases in velocity. Subsequently, the probes were used in a study of the charged particle number density and electron temperature distributions in the stagnation region of a flat-nosed cylinder in supersonic flow. The electron temperature had a constant value throughout the bow shock and the entire shock layer. The charged particle number density distribution measurements provided a graphic demonstration of the merging of the bow shock and the boundary layer at a value of Reynolds number of about 100, and also furnished evidence of the diffusive separation of the ions and atoms in the shock wave. Independent measurements of the ion flux to the stagnation point wall were in good agreement with the Langmuir probe measurements in the shock layer.
Author :North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development Publisher : ISBN 13 : Total Pages : pages Book Rating :4.0/5 ( download)
Book Synopsis Proceedings by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Download or read book Proceedings written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1957 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis UTIA Report by : University of Toronto. Institute of Aerophysics
Download or read book UTIA Report written by University of Toronto. Institute of Aerophysics and published by . This book was released on 1963 with total page 822 pages. Available in PDF, EPUB and Kindle. Book excerpt: