Reynolds Number Scaling of the Propulsive Performance of a Pitching Airfoil-Reference-Cited by-同舟云学术

Reynolds Number Scaling of the Propulsive Performance of a Pitching Airfoil

Published:2019-07 Issue:7 Volume:57 Page:2663-2669
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Senturk Utku¹,Smits Alexander J.²

Affiliation:

1. Ege University, 35040 Izmir, Turkey

2. Princeton University, Princeton, New Jersey 08544

Funder

Office of Naval Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058371

Reference9 articles.

1. Scaling the propulsive performance of heaving and pitching foils

2. GarrickI. E. “Propulsion of a Flapping and Oscillating Airfoil,” National Advisory Committee for Aeronautics Langley Memorial Aeronautical Lab. TR 567, Virginia, 1936.

3. Two‐Dimensional Problems in Hydrodynamics and Aerodynamics

4. A scaling law for thrust generating unsteady hydrofoils

5. Existence of a sharp transition in the peak propulsive efficiency of a low- pitching foil

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