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Ignition Studies of Bio-Based Fuels for Advanced Combustion EnginesJohnson, Michael Victor. January 2009 (has links)
Thesis (M.S.)--Marquette University, 2009. / Access available to Marquette University only. Scott Goldsborough, John P. Borg, Jon Kock, Henry Curran, Advisors.
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Performance of an opposed flow shock tube for the measurement of gas thermal conductivitySteenken, William G. January 1967 (has links)
Thesis (Ph. D.)--University of Wisconsin--Madison, 1967. / Typescript. Vita. Description based on print version record. Includes bibliographical references.
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Predicted scramjet testing capabilities of the proposed RHYFL-X expansion tube /Stewart, Benjamin S. January 2004 (has links) (PDF)
Thesis (Ph.D.) - University of Queensland, 2004. / Includes bibliographical references.
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Stability assessment of planetary entry vehicles in the X3 superorbital expansion tube /Abdel-Jawad, Madhat. January 2004 (has links) (PDF)
Thesis (Ph.D.) - University of Queensland, 2005. / Includes bibliography.
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Microwave studies of radiation from plasmasAro, T. O. January 1964 (has links)
No description available.
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A study of free radical processes in the chemical shock tube /Lee, William Edward January 1959 (has links)
No description available.
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Diagnostic experiments in a magnetically driven shock tube.January 1964 (has links)
No description available.
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Comparing the inviscid and viscous flows in a shock tube to analyze the boundary layer effectsSeitel, Christel M. January 2009 (has links)
Thesis (M.S.)--Rutgers University, 2009. / "Graduate Program in Mechanical and Aerospace Engineering." Includes bibliographical references (p. 105-106).
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Development of a single-stage implosion-driven hypervelocity launcherSzirti, Daniel. January 2008 (has links)
The present study deals with the development of a single-stage implosion-driven hypervelocity launcher. A thin-walled tube filled with helium surrounded by explosives acts as a driver for the launcher. Implosion of the tube drives a strong shock that reflects back and forth between the projectile and the implosion pinch, generating very high temperatures and pressures. Simple analytic models were used to approximate the performance of the pump tube and its use as a driver for a launcher. Experiments to evaluate the implosion dynamics and performance of the pump tube were carried out, and implosion-driven launcher experiments demonstrated muzzle velocities above 4 km/s with 5-mm-diameter aluminum projectiles. Projectile integrity was verified by high-speed photography. Disagreement of experimental data with the analytical models of performance is mostly due to failure to seal the chamber of the launcher, resulting in loss of driver gas, and pump tube expansion, which weakens the precursor shock.
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Kinetics and energy transfer studies using a shock tube and probe laserChenery, John A. January 1984 (has links)
A continuous wave infrared CO laser has been used to monitor kinetic processes occurring behind shock waves. Studies have been made of both vibrational energy transfer and reaction kinetics. It has been demonstrated that, following shock-heating, the vibrational levels of CO and DC1 relax via a continuous series of Boltzmann distributions into the final Boltzmann equilibrium distribution at rhe translational temperature. This is shown to be in accord with the established theory, and it is proposed that all diatomic molecules relax in this manner. Previous results for HI, which suggested otherwise, are questioned, and the theoretical arguments used to explain these results are shown to be misconceived. A new method is developed to calculate vibrational relaxation times from any laser absorption trace. The initial vibrational distribution of CO formed in the unimolecular decomposition of OCS at 4000 K has been investigated. It has been found that at least 90 % of the CO is born in the lowest vibrational level v=0, when 50 % would be in v=0 at equilibrium. This result is explained in terms of the dynamics of the reaction. The kinetics of the isotope exchange reaction <sup>12</sup>C<sup>18</sup>O + <sup>13</sup>C<sup>16>O ⥋ <sup>12</sup>C<sup>16</sup>O + <sup>13</sup>C<sup>18</sup>O have been investigated. The results have been shown to be consistent with an atomic chain mechanism, in conflict with the conclusions of earlier work. Reasons for this are discussed. A general account of the principles of operation of the apparatus is given, and conclusions are arrived at for the most profitable directions of future work.
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