Experiments were used in conjunction with a compressible flow model to investigate the temperature recovery phenomenon along a blowdown stack during a high-pressure natural gas pipeline blowdown. The test rig involved instrumented 2 in. blowdown stacks mounted on a full-bore valve. Stacks with two wall thicknesses and stagnation pressures of approximately 3000 kPa-a and 5600 kPa-g were tested, giving a total of four test cases. Using the compressible flow model, which was calibrated using static pressure measurements, the stack-gas temperature was calculated to range from −38 °C to −18 °C for the four test cases. The respective stack wall temperatures were measured to range between −13 °C and 0 °C; thus, the temperature recovery ranged between 18 °C and 26 °C. Empirical correlations available in the literature, which were developed for aeronautical applications, were tested against the experimental results. Poor agreement was found between the measured temperature recovery factor and that predicted by five empirical correlations: the coefficient of determination (R2) between the measured and correlation-calculated recovery factor was found to be negative for all five correlations.

References

1.
Canadian Standards Association (CSA)
,
2012
,
CSA Z662-11: Oil and Gas Pipeline Systems
,
CSA Group
,
Toronto
.
2.
Ackermann
,
G.
,
1942
, “
Plattenthermometer in Stroemung mit grosser Geschwindigkeit und turbulenter Grenzschicht
,”
Forsch. Ingenieurwes.
,
13
(
6
), pp.
226
234
.
3.
Seban
,
R. A.
,
1948
, “
Analysis for the Heat Transfer to Turbulent Boundary Layer in High Velocity Flow
,” Ph.D. thesis, University of California, Berkeley, CA.
4.
Shirokow
,
M.
,
1936
, “
The Influence of the Laminar Boundary Layer Upon Heat Transfer at High Velocities
,”
Tech. Phys. USSR
,
3
(
12
), p.
1020
.
5.
Squire
,
H. B.
,
1942
, “
Heat-Transfer Calculations for Aerofoils
,” British Air Ministry, Technical Report No.
1986
.
6.
Tucker
,
M.
, and
Maslen
,
S. H.
,
1951
, “
Turbulent Boundary-Layer Temperature Recovery Factor in Two-Dimensional Supersonic Flow
,” NACA, Technical Report No. 2296.
7.
Kunz
,
O.
, and
Wagner
,
W.
,
2012
, “
The GERG-2008 Wide-Range Equation of State for Natural Gases and Other Mixtures: An Expansion of GERG-2004
,”
J. Chem. Eng. Data
,
57
(
11
), pp.
3032
3091
.
8.
Lemmon
,
E. W.
,
Huber
,
M. L.
, and
McLinden
,
M. O.
,
2010
, “
NIST Standard Reference Database 23: Reference Fluid Thermodynamic and Transport Properties-REFPROP, Version 9.0
,” National Institute of Standards and Technology, Standard Reference Data Program, Gaithersburg.
9.
White
,
F. M.
,
2008
,
Fluid Mechanics
, 6th ed.,
McGraw Hill
,
New York
.
10.
Kays
,
W. M.
, and
Crawford
,
M. E.
,
1993
,
Convective Heat and Mass Transfer
, 3rd ed.,
McGraw Hill
,
New York
.
11.
Batchelor
,
B. S.
,
1967
,
An Introduction to Fluid Dynamics
,
Cambridge University Press
,
Cambridge, UK
.
12.
Idelchik
,
I. E.
,
1994
,
Handbook of Hydraulic Resistance
, 3rd ed.,
CRC Press
,
Boca Raton, FL
.
You do not currently have access to this content.