Aircraft icing
Top Cited Papers
- 15 November 2000
- journal article
- Published by The Royal Society in Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences
- Vol. 358 (1776), 2873-2911
- https://doi.org/10.1098/rsta.2000.0689
Abstract
The orbital motion of the planets in the Solar System is chaotic. As a result, initially close orbits diverge exponentially with a characteristic Lyapunov time of 5 Ma. This sensitivity to initial conditions will limit the possibility to obtain an accurate solution for the orbital and precessional motion of the Earth over more than 35 to 50 Ma. The principal sources of uncertainty in the model are review here. It appears that at present the largest source of error could reside in the lack of knowledge of the value of the precession due to the oblateness (J2) of the Sun. Nevertheless, for the calibration of geological time-scale, this limitation can be overcome to some extent if one considers in the geological data the signature of the outer planets secular orbital motion which is predictable on a much longer time-scale. Moreover, it should be possible to observe in the geological records the trace of transition from the (s4 −s3)−2(g4− g3) secular resonance to the (s4− s3)− (g4− g3) resonance. The detection and dating of these passages should induce extremely high constraints on the dynamical models for the orbital evolution of the Solar System.Keywords
This publication has 11 references indexed in Scilit:
- Ice and water film growth from incoming supercooled dropletsInternational Journal of Heat and Mass Transfer, 1999
- A 3D ice accretion simulation codePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inletPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Additional improvements to the NASA Lewis ice accretion code LEWICEPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Three-dimensional unstructured mesh procedure for iced wing flowfield and droplet trajectory calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Improvement of the ONERA 3D icing code, comparison with 3D experimental shapesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Ice accretion and performance degradation calculations with LEWICE/NSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Calculation of Flow Over Iced AirfoilsAIAA Journal, 1989
- Correlation of airfoil icing relationships with two-dimensional model and full scale rotorcraft icing test dataPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- The effect of the atmospheric droplet size distribution on aircraft ice accretionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984