Wing laminar boundary layer in the presence of a propeller slipstream
- 1 July 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (7) , 606-611
- https://doi.org/10.2514/3.45630
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Development of a Propeller Afterbody Analysis with Contracting SlipstreamPublished by SAE International ,1983
- Flight Investigation of Natural Laminar Flow on the Bellanca Skyrocket IISAE International Journal of Advances and Current Practices in Mobility, 1983