Optimization of Propeller Blade Twist by an Analytical Method
- 1 February 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 22 (2) , 252-255
- https://doi.org/10.2514/3.48441
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Factors influencing the predicted performance of advanced propeller designsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- THE EFFECT OF PROPLETS AND BI-BLADES ON THE PERFORMANCE AND NOISE OF PROPELLERSPublished by SAE International ,1981
- The effect of blade sweep on propeller performancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- A Rapidly Convergent Descent Method for MinimizationThe Computer Journal, 1963
- On the vortex theory of screw propellersProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1929