The Construction and Calibration of a Gas Shock Tube PDF Download
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Author: Skews Beric William
Publisher:
ISBN:
Category :
Languages : en
Pages : 424
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Book Description
Author: Skews Beric William
Publisher:
ISBN:
Category :
Languages : en
Pages : 424
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Book Description
Author: Charles Fleming Stebbins
Publisher:
ISBN:
Category : Shock tubes
Languages : en
Pages : 72
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Author: John Harold Roberts
Publisher:
ISBN:
Category :
Languages : en
Pages : 106
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Author: Charles F. Stebbins
Publisher:
ISBN:
Category :
Languages : en
Pages : 46
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Book Description
The tube is to be used for studying real gas phenomena in a real shock tube. The FJSRL shock tube can be fired at test pressures ranging from 1/2 micron Hg up to atmospheric pressure, with multi-test and multi-driver gas capabilities. Diaphragm pressure ratios range between 100,000 and 10 to the 8th power giving a practical range of Mach numbers, in argon, of 2
Author: S. P. Pfaff
Publisher:
ISBN:
Category : Shock tubes
Languages : en
Pages : 30
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Author: R. J. Pallant
Publisher:
ISBN:
Category : Calibration
Languages : en
Pages : 16
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Author: Theodore A. Brabbs
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 20
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Author: Stephen H. Fergason
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ISBN:
Category :
Languages : en
Pages :
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Author: Ronald E. Roll
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
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The application of the shock tube to laboratory astrophysical studies is discussed, with particular regard to the experimental determination of atomic and molecular transition probabilities. The construction of a two-inch stainless-steel shock tube and its associated mechanical and electronic equipment is described. The measurement of the pressure and velocity history of the gas flow as well as radiation measurements behind the reflected shock are discussed. A comparison of hydrodynamic observations with theoretically derived values indicates that, for the McMillin shock tube, there are deviations from accepted shock-tube behavior. Excitation temperatures computed using the emission lines of neutral iron, are found to be very much lower than can be accounted for by present shock-tube theories. (Author).
Author: Marc Finkelstein
Publisher:
ISBN:
Category : Plasma (Ionized gases)
Languages : en
Pages : 34
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