On the Effect of Rotational Forces on Rotor Blade Boundary-Layer Transition-Reference-Cited by-同舟云学术

On the Effect of Rotational Forces on Rotor Blade Boundary-Layer Transition

Published:2019-01 Issue:1 Volume:57 Page:252-266
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Weiss Armin¹,Gardner Anthony D.¹,Schwermer Till¹,Klein Christian¹,Raffel Markus¹

Affiliation:

1. DLR, German Aerospace Center, D-37073 Göttingen, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057036

Reference66 articles.

1. HeisterC. C. “Methodik zur näherungsweisen Vorhersage des laminar-turbulenten Umschlags an Hubschrauberrotoren,” Ph.D. Thesis, Univ. Stuttgart, Stuttgart, Germany, 2016. doi:10.18419/opus-8893

2. Laminar Boundary-Layer Oscillations and Stability of Laminar Flow

3. TollmienW. “The Production of Turbulence,” National Advisory Committee for Aeronautics TR NACA-TM-609, March 1931 (translation from “Nachrichten der Gesellschaft der Wissenschaften zu Göttingen,” Mathematisch-Physikalische Klasse, 1929).

4. Boundary-Layer Theory

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