Integration of Airfoil Stall and Compressibility Models into a Propeller Blade Element Model-Reference-Cited by-同舟云学术

Integration of Airfoil Stall and Compressibility Models into a Propeller Blade Element Model

Published:2016-07 Issue:4 Volume:29 Page:04016014
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Dorfling Johann¹,Rokhsaz Kamran²

Affiliation:

1. Foreign Visiting Professor, Dept. of Mechatronics and Electronics, Tecnológico de Monterrey, Guadalajara, Jalisco, Sur C.P. 64849, Mexico

2. Professor, Dept. of Aerospace Engineering, Wichita State Univ., Wichita, KS 67260-0044 (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000607

Reference56 articles.

1. Betz A. (1919). “Schraubenpropeller mit Geringstem Energieverlust.” Nachrichten der Königlichen Gesellschaft der Wissenschaften zu Göttingen Mathematisch-Physikalische Klasse Akademie der Wissenschaften in Göttingen Göttingen Germany 193–217 (in German).

2. Bober L. J. Chaussee D. S. and Kutler P. (1983). “Prediction of high speed propeller flow fields using a three-dimensional Euler analysis.” Proc. 21st AIAA Aerospace Sciences Meeting American Institute of Aeronautics and Astronautics Reston VA.

3. Bousquet J. M. and Gardarein P. (2000). “Recent improvements in propeller aerodynamic computations.” Proc. 18th AIAA Applied Aerodynamics Conf. American Institute of Aeronautics and Astronautics Reston VA.

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