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Approximate simulation of stratospheric flow from aircraft data
Author(s) -
Humi Mayer
Publication year - 2002
Publication title -
international journal for numerical methods in fluids
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.938
H-Index - 112
eISSN - 1097-0363
pISSN - 0271-2091
DOI - 10.1002/fld.437
Subject(s) - ordinary differential equation , vorticity , meteorology , flow (mathematics) , path (computing) , initial value problem , physics , mathematics , mechanics , environmental science , mathematical analysis , differential equation , computer science , vortex , programming language
Abstract We show how stratospheric data collected by an aircraft along its flight path can be used to initialize steady state approximate simulations of the stratospheric flow. To this end we reformulate the initial value problem for Boussinesq equations as a large system of stiff ordinary differential equations (using the method of lines). Initial conditions for this system are derived from the aircraft data. As a result we are able to compute the Brunt–Vaisala frequency, Richardson number and the vorticity in the vicinity of the flight path. Copyright © 2003 John Wiley & Sons, Ltd.