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Dimensioning of cryogenic transfer lines

โœ Scribed by M.V. Krishna Murthy; R.V. Seshagiri Rao; K. Srinivasan


Publisher
Elsevier Science
Year
1974
Tongue
English
Weight
318 KB
Volume
14
Category
Article
ISSN
0011-2275

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โœฆ Synopsis


Nomenclature a acoustic velocity in vapour at temperature Ta, m s "1 Cp specific heat, kcal kg "1 K "l d diameter of the pipe when vents are provided on the line, m D diameter of the pipe line when vents are not provided, m (unless mentioned otherwise) gc gravitational constant 9.81 kg ms "2 kgf q K I constant deemed in (11) K2 constant defined in (23) L length of the pipe line, m LI interval between the vents, m P pressure, lb in'aa Q volumetric flow rate, m a s "I (unless mentioned otherwise) R gas constant, kgfm kg q K q T a ambient temperature assumed to be 300 K Tn temperature deemed in (13) T s saturation temperature of liquid at one atmosphere, K u velocity, m s "1 v specific volume, m a s q x distance along the pipe line from entrance, m r shear stress, lb in-2 p density, kg m "a 3' ratio of specific heats Subscripts d with vents provided f liquid g vapour min minimum v vent


๐Ÿ“œ SIMILAR VOLUMES


Cool-down studies on vacuum insulated cr
โœ M.V. Krishna Murthy; S. Srinivasa Murthy; K. Srinivasan; M. Kanniah ๐Ÿ“‚ Article ๐Ÿ“… 1976 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 300 KB

Analytical and experimental studies on the cool-down of vacuum insulated cryogenic transfer lines have been carried out. An expression for estimating the cool-down history is derived taking into account the gas conduction effects. Experiments were carried out for LN2 flow in glass lines. The cool-do

Analytical and experimental investigatio
โœ K. Srinivasan; V. Seshagiri Rao; M.V. Krishna Murthy ๐Ÿ“‚ Article ๐Ÿ“… 1974 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 484 KB

Cool-down of cryogenic transfer lines is studied analytically and experimentally. Analytical expressions are derived for estimating cool-down time of uninsulated and vacuum insulated lines. The experimental results prove that for short sections the mass flow-rate does not affect the cool-down very s