Mechanisms Influencing the Efficiency of Oscillating Airfoil Propulsion
By John Young, Joseph C. S. Lai. 2007
162 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/984b021141eeff2e85a0f4eb069573ac25beaf0a
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
In Computational Mechanics
- Max F. Platzer
- John Young
- Joseph C. S. Lai
- K. Jones
- Alexander J Smits
- Ivan Marusic
- B. McKeon
- Marcus Hultmark
Citations in the corpus
- Flapping Wing Aerodynamics: Progress and Challenges (2008, methodology): “However, Navier–Stokes computations byYoung and Lai [24,25] for the same airfoil in incompressible flow in the Reynolds number range between 10,000 to 30,000 reveals significant differences compared with the high-Reynolds number behavior.”
- Undulatory and oscillatory swimming (2019, background): “This limit of the angle of attack suggests that leading edge vortex formation and dynamic stall effects need to be avoided to achieve the best performance (Tuncer & Kaya 2005; Young et al. 2006; Young & Lai 2007).”