A Method of Airplane Performance Calculation Applicable to Any Polar
- 1 April 1947
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 14 (4), 243-252
- https://doi.org/10.2514/8.1329
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Nondimensional Buckling Curves-Their Development and ApplicationJournal of the Aeronautical Sciences, 1946
- Secant Modulus Method for Determining Plate Instability Above the Proportional LimitJournal of the Aeronautical Sciences, 1946
- A Tabular Method of Propeller Blade Stress AnalysisJournal of the Aeronautical Sciences, 1943