Unsteady low-speed aerodynamic model for complete aircraft configurations
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California
2. Analytical Methods Inc., Redmond, Washington
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45564
Reference41 articles.
1. Computational Aerodynamics Development and Outlook
2. Analysis and design of wing-body combinations at subsonic and supersonic speeds.
3. Calculation of potential flow about arbitrary bodies
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