Minimum Trimmed Drag and Optimum c.g. Position
Author:
Affiliation:
1. Hochshule der Bundeswehr Munchen, Neubiberg, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58390
Reference12 articles.
1. Some Trim Drag Considerations for Maneuvering Aircraft
2. Hofmann, L.G. and Clement, W.F. "Vehicle Design Considerations for Active Control Applications to Subsonic Transport Aircraft,"NASA CR-2408, 1974.
3. Trimmed drag considerations
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