Wind-Tunnel Investigation of Air Flow Over a Hexadecanol Monolayer Spread on a Water Surface

1968 ◽  
Vol 11 (4) ◽  
pp. 0553-0557
Author(s):  
W. F. Schwiesow and F. R. Crow
Keyword(s):  
2020 ◽  
Vol 32 (12) ◽  
pp. 125120
Author(s):  
María Jiménez-Portaz ◽  
Luca Chiapponi ◽  
María Clavero ◽  
Miguel A. Losada

2021 ◽  
Vol 73 (04) ◽  
pp. 35-36
Author(s):  
Chris Carpenter

This article, written by JPT Technology Editor Chris Carpenter, contains highlights of paper OTC 30646, “Experimental Investigation of LNG Underwater Release and Combustion Behavior on the Water Surface,” by Yixiang Zhang, Jianlu Zhu, and Youmei Peng, China University of Petroleum, et al., prepared for the 2020 Offshore Technology Conference, originally scheduled to be held in Houston, 4-7 May. The paper has not been peer reviewed. Copyright 2020 Offshore Technology Conference. Reproduced by permission. Most liquefied natural gas (LNG) is transported by ship, creating opportunities for potential hazards to surrounding devices and the environment. Nevertheless, few studies have examined the characteristics of LNG underwater leakage and subsequent vapor flame. The paper considers transportation safety and risk evaluation for LNG, with emphasis on accidental release and vapor flame. Introduction The cryogenic nature of LNG, with a boiling point of -162°C, raises safety concerns with regard to vaporization gas hazards and the potential for pool fires. According to the literature devoted to LNG accidental release and spill, three puncture positions have been proposed: Category I, where the leakage point is above the water line; Category II, where the point is at or close to the water line; and Category III, where the point is below the water line. A need exists to investigate LNG underwater leakage and combustion behavior for risk assessment. This work focuses on experimental research of the dynamic behavior of LNG jet release under water and the immediate burning on the water surface using three orifices and different crosswinds. The main points of investigation include the following: - Liquid-rising process and microbehavior in the orifice - Flame geometry on the water surface under crosswinds - Flame-temperature distribution on the water surface Experimental Setup Experimental Facilities. Experiments were conducted in a rectangular tank measuring 1000 mm long, 500 mm wide, and 500 mm high, which was placed in a wind tunnel. The nozzles have diameters of 1, 3, and 5 mm in the middle of the discharge pipe. An inline cryogenic flow-meter with a measuring range of 0.06 - 0.6 m3/h was used to regulate the volume flow rate with an accuracy of 1.5 %. The pressure measurements were performed by a pressure gauge with a range from 0 to 4 MPa placed on the end of the discharged pipeline. The LNG jets were re-leased vertically into the bulk water at a depth of 0.6 m. Images were recorded using a high-speed video camera system. Experimental Conditions. The window was closed when LNG was released, and the discharged gas was quickly diffused from the wind tunnel. The temperature in the room was 17±1°C and 14±0.5°C in water. The relative humidity was approximately 50%. All tests were conducted three times.


2008 ◽  
Vol 2 (3) ◽  
pp. 340-345 ◽  
Author(s):  
Zhizhong Li ◽  
Shengli Wu ◽  
Janis Dale ◽  
Lin Ge ◽  
Mudan He ◽  
...  

2019 ◽  
Author(s):  
Vitalii Yanovych ◽  
Daniel Duda ◽  
Vít Horáček ◽  
Václav Uruba

1963 ◽  
Vol 16 (4) ◽  
pp. 475 ◽  
Author(s):  
LM Fitzgerald

A laboratory wind tunnel has been used to study the effect of wind on a water surface. The surface shearing stress 7'0 and the slope of the surface induced by wind have been measured. Values of the surface stress, in good agreement with each other, have been obtained from: (a) the velocity profile of the wind above the water surface, (b) the measured values of surface slope or set-up, and (c) the spreading characteristics of surface films. The drag coefficient, Cn = TO/ pu2n, was found to be constant for wind speeds up to about 412 cm/s and then to rise gradually for higher wind speeds.


2017 ◽  
pp. 353-358
Author(s):  
S. Castellano ◽  
G. Starace ◽  
L. De Pascalis ◽  
M. Lippolis ◽  
G. Scarascia Mugnozza
Keyword(s):  

2020 ◽  
Author(s):  
Oleg Druzhinin

<p>The objective of the present study is to investigate sensible and latent heat transfer mediated by evaporating saline droplets in a turbulent air flow over a waved water surface by performing direct numerical simulation. Equations of the air-flow velocity, temperature and humidity are solved simultaneously with the two-way-coupled equations of individual droplets coordinates and velocities, temperatures and masses. Two different cases of air and water surface temperatures,T<sub>a</sub> = 27 <sup>0</sup>C, T<sub>s</sub> = 28 <sup>0</sup>C,  and T<sub>a</sub> = -10 <sup>0</sup>C, T<sub>s</sub> = 0 <sup>0</sup>C, are considered and conditionally termed as "tropical cyclone" (TC) and "polar low"  (PL) conditions, respectively. Droplets-mediated sensible and latent heat fluxes, Q<sub>S</sub> and Q<sub>L</sub>, are integrated along individual droplets Lagrangian trajectories and evaluated as distributions over droplet diameter at injection, d, and also obtained as Eulerian, ensemble-averaged fields. The results show that under TC-conditions, the sensible heat flux from droplets to air is negative whereas the latent heat flux is positive, and thus droplets cool and moisturize the carrier air. On the other hand, under PL-conditions, Q<sub>S</sub> and Q<sub>L</sub>  are both positive, and Q<sub>L</sub> – contribution is significantly reduced as compared to Q<sub>S</sub> - contribution. Thus in this case, droplets warm up the air. In both cases, the droplet-mediated enthalpy flux, Q<sub>S</sub><sub> </sub>+ Q<sub>L </sub>, is positive, vanishes for sufficiently small droplets (with diameters d ≤ 150 μm) and further increases with d. The results also show that the net fluxes are reduced with increasing wave slope.</p><p>This work is supported by the Ministry of Education and Science of the Russian Federation (Task No. 0030-2019-0020). Numerical algorithms were developed under the support of RFBR (Nos. 18-05-60299, 18-55-50005, 18-05-00265, 20-05-00322). Postprocessing was performed under the support of the Russian Science Foundation (No. 19-17-00209).</p>


1947 ◽  
Vol 157 (1) ◽  
pp. 482-497 ◽  
Author(s):  
K. W. Todd

This paper deals mainly with the development of a high-speed wind tunnel for the testing of turbine or compressor blade cascades under two-dimensional air flow at velocities up to that of sound. It includes a brief résumé of the early history of the technique, and goes on to enumerate the variables which must be brought under the operator's control. Reference is made to methods of presentation of results, including the use of optical systems for demonstration of shock phenomena. Finally, the control system evolved for operating the high-speed tunnel is described, and some notes are added on the protection of the operators from fatigue induced by monotony and noise.


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