Comparison of Aircraft Conceptual Design Weight Estimation Methods to the Flight Optimization System
Author:
Affiliation:
1. NASA Langley Research Center
2. Self
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2032
Reference7 articles.
1. Minimizing life cycle cost for subsonic commercial aircraft
2. Aircraft Design: A Conceptual Approach, Fifth Edition
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