An experimental low Reynolds number comparison of a Wortmann FX67-K170 airfoil, a NACA 0012 airfoil, and a NACA 64-210 airfoil in simulated heavy rain
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1987
Main Author: | Craig, Anthony Paul. |
---|---|
Other Authors: | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. |
Format: | Thesis |
Published: |
Massachusetts Institute of Technology
2023
|
Subjects: | |
Online Access: | https://hdl.handle.net/1721.1/150505 |
Similar Items
-
Reynolds number effects on the unsteady aerodynamic behavior of an NACA 0012 airfoil
by: Fletcher, Michael Joseph.
Published: (2023) -
Dynamic stall of a NACA 0012 airfoil in laminar flow
by: Digavalli, Sasi K. (Sasi Kumar)
Published: (2005) -
Aerodynamic Characteristics Of Membrane Airfoil Compared To Rigid Naca 4412 Airfoil
by: Chan, Min Xhao
Published: (2018) -
Shedding vortex characteristics analysis of NACA 0012 airfoil at low Reynolds numbers
by: Jianlong Chang, et al.
Published: (2022-07-01) -
Numerical investigation on NACA0012 airfoil with tubercular structure
by: Açıkel Halil Hakan, et al.
Published: (2022-01-01)