Analytical Model for Ring-Wing Propulsors at Angle of Attack-Reference-Cited by-同舟云学术

Analytical Model for Ring-Wing Propulsors at Angle of Attack

Published:2022-09 Issue:5 Volume:59 Page:1351-1362
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Werle Michael J.¹^ORCID

Affiliation:

1. Halo Energy LLC, Wellesley, Massachusetts 02481

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C036326

Reference28 articles.

1. Aerodynamic Loads and Moments on Axisymmetric Ring-Wing Ducts

2. WerleM. J. “Aerodynamic Loads and Moments for Ring Wing Ducts,” Ogin Energy Corp. Rept. Ogin-0060, Waltham, MA, Sept, 2013.

3. FletcherH. S. “Experimental Investigation of Lift, Drag and Pitching Moment of Five Annular Airfoils,” NACA TN 4117, 1957.

4. RyallD. L.CollinsI. F. “Design and Test of a Series of Annular Airfoils,” Admiralty Research Lab. Rept. A.R.L./R3/G/AE/2/5, ARL/G/R6, Teddington, England, U.K. March 1965, https://reports.aerade.cranfield.ac.uk/handle/1826.2/4069.

5. MorganW. B.CasterE. B. “Prediction of the Aerodynamic Characteristics of Annular Airfoils,” David Taylor Model Basin Rept.1830, Carderock, MD, Jan. 1965, http://hdl.handle.net/1721.3/49012.

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