Computation of Influence Coefficients for Aircraft Structures with Discontinuities and Sweepback
- 1 October 1947
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 14 (10) , 547-560
- https://doi.org/10.2514/8.1454
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- The Applicability of Saint-Venant's Principle to Airplane StructuresJournal of the Aeronautical Sciences, 1945
- Stress Analysis of Nondevelopable Semimonocoque Structures Considered as Beams of Variable SectionJournal of the Aeronautical Sciences, 1945
- Vibrations of Composite StructuresJournal of the Aeronautical Sciences, 1945
- A New Method of Calculating Natural Modes of Uncoupled Bending Vibration of Airplane Wings and Other Types of BeamsJournal of the Aeronautical Sciences, 1944
- Three-Dimensional Flutter AnalysisJournal of the Aeronautical Sciences, 1941
- Least Work Solutions of Shear Lag ProblemsJournal of the Aeronautical Sciences, 1941
- Unit Method of Beam AnalysisJournal of the Aeronautical Sciences, 1941