A Mixed Optimization Method for Automated Design of Fuselage Structures
- 1 December 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (12) , 805-811
- https://doi.org/10.2514/3.59080
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Airbreathing Launch Vehicle for Earth Orbit Shuttle-Performance and OperationJournal of Aircraft, 1971
- Procedure for Automating Aircraft Wing Structural DesignJournal of the Structural Division, 1971
- Über die Tragfähigkeit eines längsbelasteten Plattenstreifens nach Überschreiten der Beullast.ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1937