Coupled Boundary-Layer Suction and Airfoil Optimization for Hybrid Laminar Flow Control-Reference-Cited by-同舟云学术

Coupled Boundary-Layer Suction and Airfoil Optimization for Hybrid Laminar Flow Control

Published:2021-12 Issue:12 Volume:59 Page:5158-5173
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Sudhi Anand¹^ORCID,Elham Ali¹,Badrya Camli¹^ORCID

Affiliation:

1. Technical University of Braunschweig, 38108 Braunschweig, Germany

Funder

Deutsche Forschungsgemeinschaft

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060480

Reference32 articles.

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2. DareckM.EdelstennC.EnderT. “Flightpath 2050 Europe’s Vision for Aviation,” Report of the High Level Group on Aviation Research TR, Vol. 98, Publications Office of the European Union, Luxembourg, 2011, p. 28, https://ec.europa.eu/transport/sites/default/files/modes/air/doc/flightpath2050.pdf [retrieved 15 Aug. 2020].

3. Drag Reduction by Laminar Flow Control

4. Aerodynamic considerations of blended wing body aircraft

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