Low-Reynolds-number airfoil design for the M.I.T. Daedalus prototype- A case study
- 1 August 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (8) , 724-732
- https://doi.org/10.2514/3.45650
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Viscous-inviscid analysis of transonic and low Reynolds number airfoilsAIAA Journal, 1987
- Flight Research with the MIT Daedalus PrototypePublished by SAE International ,1987
- ISES - A two-dimensional viscous aerodynamic design and analysis codePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- On displacement thicknessJournal of Fluid Mechanics, 1958