Calibration of the Tailored Interface 8" X 10" Shock Tunnel PDF Download
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Author: A. Kuritzky
Publisher:
ISBN:
Category :
Languages : en
Pages : 82
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Author: A. Kuritzky
Publisher:
ISBN:
Category :
Languages : en
Pages : 82
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 87
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Book Description
The work presents the design considerations and the calibration of a shock tunnel for aerodynamic measurements at hypersonic Mach numbers. The shock tunnel is composed of a shock tube which is used for the production of high temperature and high pressure air reservoir, which is then expanded through a supersonic nozzle, thereby attaining high Mach number flow in the test section. In order to obtain maximum test time a 'tailored' mode of operation is used for this shock tunnel. A method for calculating the optimum ratio of the compression Chamber length to the low pressure tube length for a given total shock tube length that will result in a maximum test duration is presented. The flow in the test section is calibrated using a total pressure rake and by static pressure measurements and measurements of stagnation point heat transfer rates at various points in the test section. The flow conditions are then calculated using the theoretical relations for stagnation point heat transfer rates. The experimental results show the flow in the horizontal plane with a relatively thin boundary layer.
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 994
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Author:
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ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 804
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Author: 陳俊岳
Publisher:
ISBN:
Category :
Languages : en
Pages : 87
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Author:
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ISBN:
Category : Plasma (Ionized gases)
Languages : en
Pages : 634
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Author: Kazuyoshi Takayama
Publisher: Springer Science & Business Media
ISBN: 3642776485
Category : Science
Languages : en
Pages : 735
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Book Description
Shock wave research covers important inderdisciplinary areas which range from basic topics on gasdynamics, combustion and detonation, physico-chemistry of high temperature gases, plasma physics, astro and geophysics, materials science, astronautics and space technology to medical and industrial applications. This book includes 202 papers presented at the 18th the International Symposium on Shock Waves which describe the research frontier of shock wave phenopmena and 14 plenary lectures which show the state of the art of various fields of shock wave research. This proceedings is a unique collection of most important and updated shock wave research.
Author: James T. Curtis
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 176
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A combined analytical and experimental investigation of the effect of stagnation region chemicalionization non-equilibrium phenomena on the aerothermodynamic and electrical properties of the flow field over a hemisphere cylinder at hypersonic speeds was conducted. In the analytical studies, flow field caluclations were made using several IBM 704 computer programs which account for finite reaction rate processes. The experimental phases of the study were done in the Cornell Aeronautical Laboratory 6' Shock Tunnel at a nominally constant velocity of 15,500 ft/sec. Measurements were made of the surface pressure and heat transfer, shock layer pitot pressure, and suface layer electrical conductivity on hemishpere cylinder models for a range of values of the stagnation region non-equilibrium scaling parameter. (Author).
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 584
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 134
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