Use of a Certification Constraints Module for Aircraft Design Activities
Author:
Affiliation:
1. ONERA
2. Higher Institute of Aeronautics and Space
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3762
Reference33 articles.
1. Development of NOVA Aircraft Configurations for Large Engine Integration Studies
2. Multifidelity Conceptual Design and Optimization of Strut-Braced Wing Aircraft using Physics Based Methods
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