What is it about?
The main objective of this work is to show appropriated available methodologies used to calculate and modeling aerodynamic coefficients in the distinct aircraft design phases. Other objective is to present the main recommended practices and general structure of the aerodynamic model to attend the requirements of different technologies during design cycles, such as Loads and Flight Dynamics.
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Why is it important?
This work shows how to get longitudinal aerodynamic coefficients and derivatives from wind tunnel tests, theoretical and empirical methods. It will focus on methodologies and techniques that are in public domain and are easy to be used.
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This page is a summary of: Aerodynamic Longitudinal Coefficient Modeling During Aircraft Design Phases, June 2016, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2016-4133.
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