An Interferometric Investigation of Shock Structure and Its Induced Shock-tube Boundary Layer in Ionized Argon PDF Download
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Author: University of Toronto. Institute for Aerospace Studies Publisher: Institute for Aerospace Studies, University of Toronto ISBN: Category : Boundary layer Languages : en Pages : 69
Book Description
The structure of ionizing shock waves and their induced boundary layers in argon have been studied experimentally in the UTIAS 4 inch x 7 inch hypervelocity shock tube using dual-wavelength interferometry. The relaxation lengths and transitions of shocks of Mach numbers 16.5 and 13.5 for initial gas pressures of about 5 torr have been measured at 2cm and 8cm, respectively. The transition profiles and relaxation lengths are in reasonably good agreement with analysis.
Author: University of Toronto. Institute for Aerospace Studies Publisher: Institute for Aerospace Studies, University of Toronto ISBN: Category : Boundary layer Languages : en Pages : 69
Book Description
The structure of ionizing shock waves and their induced boundary layers in argon have been studied experimentally in the UTIAS 4 inch x 7 inch hypervelocity shock tube using dual-wavelength interferometry. The relaxation lengths and transitions of shocks of Mach numbers 16.5 and 13.5 for initial gas pressures of about 5 torr have been measured at 2cm and 8cm, respectively. The transition profiles and relaxation lengths are in reasonably good agreement with analysis.
Author: Wade H. Shafer Publisher: Springer Science & Business Media ISBN: 1475757824 Category : Science Languages : en Pages : 304
Book Description
Masters Theses in the Pure and Applied Sciences was first conceived, published, and dis seminated by the Center for lnformation and Numerica/ Data Analysis and Synthesis (C/NDAS) * at Purdue University in 1957, starting its coverage of theses with the academic year 1955. Beginning with Volume 13, the printing and dissemination phases of the ac tivity were transferred to University Microfilms/Xerox of Ann Arbor, Michigan, with the thought that such an arrangement would be more beneficia! to the academic and general scientific and technical community. After fi ve years of this joint undertaking we had concluded that it was in the interest of ali concerned if the printing and distribution of the volume were handled by an international publishing house to assure improved service and broader dissemination. Hence, starting with Volume 18, Masters Theses in the Pure and App/ied Sciences has been disseminated on a worldwide basis by Plenum Publishing Corporation of New York, and in the same year the coverage was broadened to include Canadian universities. Ali back issues can also be ordered from Plenum. We have reported in Volume 21 (thesis year 1976) a total of 10,586 theses titles from 25 Canadian and 219 United States universities. We are sure that this broader base for theses titles reported will greatly enhance the value of this important annual reference work.
Author: K. Takayama Publisher: ISBN: Category : Boundary layer Languages : en Pages : 27
Book Description
Analyses are made of the mutual interactions between shock structure and the sidewall laminar boundary-layer and their effects on the quasi-steady flat-plate laminar boundary layer in ionizing argon shock-tube flows. The mutual interactions are studied using effective quasi-one-dimensional equations derived from an area-averaged-flow concept in a finite-area shock tube. The effects of mass, momentum and energy non-uniforities and the wall dissipations in the ionization and relaxation regions on the argon shock structure are discussed. The new results obtained for shock structure, shock-tube laminar sidewall and quasi-steady flat-plate boundary-layer flows are compared with dual-wavelength interferometric data obtained from utias 10 cm x 18 cm Hypervelacity Shock Tube.
Author: University of Toronto. Institute for Aerospace Studies
Author: University of Toronto. Institute for Aerospace Studies
Author: University of Toronto. Institute of Aerospace Studies
Author: Wade H. Shafer
Author: 
Author: K. Takayama
Author: University of Toronto. Institute for Aerospace Studies
Author: Liu, W. S
Author: 
Author: Theodore A. Brabbs
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