MODIFICATION OF THE FUCHS CONDENSATION THEORY TO PREDICT TRANSITIONAL CONDENSATIONAL GROWTH OF NON-SPHERICAL ICE PARTICLES

2001 ◽  
Vol 32 ◽  
pp. 1039-1040
Author(s):  
A.B. NADYKTO ◽  
E.R. SHCHUKIN ◽  
M. KULMALA ◽  
A. LAAKSONEN
2015 ◽  
Vol 72 (9) ◽  
pp. 3293-3308 ◽  
Author(s):  
Joachim Jansen ◽  
Andrew J. Heymsfield

Abstract Aerodynamic condensation is a result of intense adiabatic cooling in the airflow over aircraft wings and behind propeller blades. Out of cloud, condensation appears as a burstlike fog (jet aircraft during takeoff and landing, propellers) or as an iridescent trail visible from the ground behind the trailing edge of the wing (jet aircraft in subsonic cruise flight) consisting of a monodisperse population of ice particles that grow to sizes comparable to the wavelength of light in ambient humidities above ice saturation. In this paper, the authors focus on aerodynamic contrail ice particle formation processes over jet aircraft wings. A 2D compressible flow model is used to evaluate two likely processes considered for the initial ice particle formation: homogeneous droplet nucleation (HDN) followed by homogeneous ice nucleation (HIN) and condensational growth of ambient condensation nuclei followed by their homogenous freezing. The model shows that the more numerous HDN particles outcompete frozen solution droplets for water vapor in a 0.5–1-m layer directly above the wing surface and are the only ice particles that become visible. Experimentally verified temperature and relative humidity–dependent parameterizations of rates of homogeneous droplet nucleation, growth, and freezing indicate that visible aerodynamic contrails form between T = −20° and −50°C and RH ≥ 80%. By contrast, combustion contrails require temperatures below −38°C and ice-saturated conditions to persist. Therefore, aerodynamic and combustion contrails can be observed simultaneously.


1988 ◽  
Vol 34 (118) ◽  
pp. 318-326 ◽  
Author(s):  
Ian J. Jordaan ◽  
Garry W. Timco

Abstract During fast indentation tests on ice sheets at constant rates, crushing is commonly observed at appropriate combinations of speed and aspect ratio. An analysis is made of this mode of failure, using as a basis a recently conducted test on an ice sheet under controlled conditions. The variation of load with time is given special attention, and cyclic variation of load is associated with periodic crushing (pulverization) events, followed by clearing of the crushed ice particles. An analysis of the clearing process is summarized in the paper, treating the crushed ice as a viscous material. A detailed analysis of the energy exchanges during the indentation process is given. Elastic variations of stored energy in the indenter and in the ice sheet are calculated; these are relatively minor. The dissipation of energy during a typical load cycle (3 mm movement during 0.05 s) is about 8 J. The energy required to create surfaces of the crushed ice particles is small (0.006 J), as is the work of crushing based on mechanical testing (0.09 J). It is concluded that the process of viscous extrusion of crushed ice is the main seat of energy dissipation, basically as a frictional process. A relationship for the mean thickness of the crushed ice layer is developed, based on energy-balance considerations.


2020 ◽  
pp. 128296
Author(s):  
Ruijie Cao ◽  
Renhui Ruan ◽  
Houzhang Tan ◽  
Shengjie Bai ◽  
Yongle Du ◽  
...  

2019 ◽  
Vol 145 ◽  
pp. 105953 ◽  
Author(s):  
M. Reitzle ◽  
S. Ruberto ◽  
R. Stierle ◽  
J. Gross ◽  
T. Janzen ◽  
...  

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