The Integrated Use of Analog and Digital Computing Machines for Aircraft Dynamic Load Problems
- 1 August 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (8) , 721-740
- https://doi.org/10.2514/8.3647
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- The Static Stability of a Two-Dimensional Curved Panel in a Supersonic Flow, with an Application to Panel FlutterJournal of the Aeronautical Sciences, 1954
- Analysis of Flutter in Compressible Flow of a Panel on Many SupportsJournal of the Aeronautical Sciences, 1954
- An Exact Solution for Two-Dimensional Linear Panel Flutter at Supersonic SpeedsJournal of the Aeronautical Sciences, 1954
- Some remarks on radiation conditionsPublished by American Mathematical Society (AMS) ,1954
- Beam-Vibration Analysis With the Electric-Analog ComputerJournal of Applied Mechanics, 1950