Temperature Gradients in Turbulent Gas Streams (Effect of Flow Conditions Upon Eddy Conductivity)

1956 ◽  
Vol 48 (12) ◽  
pp. 2218-2223 ◽  
Author(s):  
N. T. Hsu ◽  
Kazuhiko. Sato ◽  
B. H. Sage
Keyword(s):  
Temperature Gradients ◽  
Flow Conditions ◽  
Gas Streams

Temperature Gradients in Turbulent Gas Streams - Behavior Near Boundary in Two Dimensional Flow.

1953 ◽  
Vol 45 (10) ◽  
pp. 2139-2145 ◽  
Author(s):  
S. D. Cavers ◽  
N. T. Hsu ◽  
W. G. Schlinger ◽  
B. H. Sage
Keyword(s):  
Temperature Gradients ◽  
Two Dimensional ◽  
Gas Streams ◽  
Dimensional Flow ◽  
Two Dimensional Flow

TEMPERATURE GRADIENTS IN TURBULENT GAS STREAMS. METHODS AND APPARATUS FOR FLOW BETWEEN PARALLEL PLATES

1952 ◽  
Vol 44 (2) ◽  
pp. 410-419 ◽  
Author(s):  
W. H. Corcoran ◽  
F. Page ◽  
W. G. Schlinger ◽  
B. H. Sage
Keyword(s):  
Temperature Gradients ◽  
Parallel Plates ◽  
Gas Streams

Temperature Gradients in Turbulent Gas Streams

1953 ◽  
Vol 45 (3) ◽  
pp. 662-666 ◽  
Author(s):  
W. G. Schlinger ◽  
V. J. Berry ◽  
J. L. Mason ◽  
B. H. Sage
Keyword(s):  
Temperature Gradients ◽  
Gas Streams

Temperature Gradients in Turbulent Gas Streams - Recovery Factors in Steady, Uniform Flow

1955 ◽  
Vol 47 (6) ◽  
pp. 1243-1248
Author(s):  
J. B. Opfell ◽  
Kazuhiko Sato ◽  
B. H. Sage
Keyword(s):  
Uniform Flow ◽  
Temperature Gradients ◽  
Gas Streams

Temperature Gradients in Turbulent Gas Streams. Measurement of Temperature, Energy, and Pressure Gradients.

1953 ◽  
Vol 45 (4) ◽  
pp. 864-870 ◽  
Author(s):  
W. G. Schlinger ◽  
N. T. Hsu ◽  
S. D. Cavers ◽  
B. H. Sage
Keyword(s):  
Temperature Gradients ◽  
Pressure Gradients ◽  
Gas Streams

Bowing of Cryogenic Pipelines

1961 ◽  
Vol 28 (3) ◽  
pp. 409-416 ◽  
Author(s):  
W. G. Flieder ◽  
J. C. Loria ◽  
W. J. Smith
Keyword(s):  
Thermal Stress ◽  
Thermal Stresses ◽  
Temperature Gradients ◽  
Stress Distributions ◽  
Flow Conditions ◽  
Additional Consideration ◽  
Dead Weight ◽  
Circular Arc ◽  
Cryogenic Fluids

The design of propellant loading systems for present-day missiles involves the design of pipelines that can carry cryogenic fluids and requires an additional consideration beyond the conventional analyses for flexibility and dead weight. Because of varying flow conditions and boil-off, these cryogenic lines experience varying fill levels and concomitant temperature gradients which cause these lines to bow; i.e., to assume a uniform curvature of circular arc. If constrained, the thermal-stress distributions which are generated by the temperature gradients will have superposed on them additional stresses, which result from the action of the support constraints. This combination of stresses may be critical and/or the loads on the supports may be excessive. The following analysis investigates these bowing effects, thermal stresses, and indicates the support problems entailed.

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