Applications of similar solutions for calculation of laminar boundary-layer characteristics in the presence of a pressure gradient.
- 1 April 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (4) , 799-801
- https://doi.org/10.2514/3.4069
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Damping of Flexural Vibrations of Sandwich PlatesJournal of the Aerospace Sciences, 1962
- Simplified Vibration Analysis of Elastic Sandwich PlatesJournal of the Aerospace Sciences, 1960
- Flexural Vibrations of Elastic Sandwich PlatesJournal of the Aerospace Sciences, 1960