General equations of motion for an elastic wing and method of solution
Author:
Affiliation:
1. Saab Scania AB, Linkoping, Sweden
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8750
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1. Über die Entstehung des dynamischen Auftriebes von Tragflügeln
2. Transient lift of three-dimensional purely supersonic wings
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