The Second-Order Compressibility Rule for Airfoils
- 1 September 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (9) , 647-648
- https://doi.org/10.2514/8.3165
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- The Minimum Weight Design of Wings for Flutter ConditionsJournal of the Aeronautical Sciences, 1953
- An Experimental Study of Natural Vibrations of Cantilevered Triangular PlatesJournal of the Aeronautical Sciences, 1953
- Vibration of Rectangular and Skew Cantilever PlatesJournal of Applied Mechanics, 1951
- Effect of Torsional Stiffness Requirements on Wing Structural WeightJournal of the Aeronautical Sciences, 1950