An unsteady vortex-ring model for microburst simulation-Reference-Cited by-同舟云学术

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An unsteady vortex-ring model for microburst simulation

Published:1989-01-09 Issue: Volume: Page:
ISSN:
Container-title:27th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

WAN TUNG¹,PAYNE FRED²

Affiliation:

1. California Polytechnic State University, San Luis Obispo

2. Texas, University, Arlington

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1989-811

Reference18 articles.

1. Fujita, T. T. "Spearhead echo and downburst near - the approach end of a John F. Kennedy airport runway,NYC',Satellite&MesometeorologyResearch Project, 137,Dept. of the Geophysical Sciences,Univ. of Chicago, 1976.

2. Bray, R. S. "Asimple microburstwind model f@ruse inpilotedsimulation",AIM22ndAerospaceSciences Meeting, Report 0357,Jan. 1984.

3. Zhu, S., and B. Etkin, "Fluid dynamic model of a downburst", UTIAS Report 271, Institute for Aerospace Studies,Univ. of Toronto, 1983.

4. A ring-vortex downburst model for flight simulations

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3. Development and application of an integral method for the incompressible Navier-Stokes equations;Mathematical and Computer Modelling;1990

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