Abstract

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference -- 16 August 2004 through 19 August 2004 -- Providence, RI -- 64922

Aerodynamic and propulsive modeling of current aircraft fleet is vital for Air Traffic Management applications, especially for use in decision support tools to predict aircraft trajectories and simulation tools. There are various models already in use or proposed. A different aerodynamic and propulsive modeling is presented in this paper. The new model considers the compressibility effects and non-linear variations of the drag polar. In addition, the thrust and specific fuel consumption models proposed consider variations of these quantities both with altitude and the Mach number. Copyright © 2004 by the American Institute of Aeronautics and Astronautics, Inc.


Original document

The different versions of the original document can be found in:

http://dx.doi.org/10.2514/6.2004-4792
https://academic.microsoft.com/#/detail/2128892861
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Document information

Published on 15/08/04
Accepted on 15/08/04
Submitted on 15/08/04

Volume 2004, 2004
DOI: 10.2514/6.2004-4792
Licence: CC BY-NC-SA license

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