Leading-Edge Vortex Interactions at a Generic Multiple Swept-Wing Aircraft Configuration-Reference-Cited by-同舟云学术

Leading-Edge Vortex Interactions at a Generic Multiple Swept-Wing Aircraft Configuration

Published:2019-11 Issue:6 Volume:56 Page:2093-2107
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Pfnür Stefan¹,Breitsamter Christian¹

Affiliation:

1. Technical University of Munich, 85748 Garching, Germany

Funder

Deutsche Forschungsgemeinschaft

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference26 articles.

1. ChambersJ. R.AnglinE. L. “Analysis of Lateral-Directional Stability Characteristics of a Twin-Jet Fighter Airplane at High Angles of Attack,” NASA TN-D-5361, Aug. 1969.

2. GreerH. D. “Summary of Directional Divergence Characteristics of Several High-Performance Aircraft Configurations,” NASA TN-D-6993, Nov. 1972.

3. Use of hinged strakes for lateral control at high angles of attack

4. Forebody vortex management for yaw control at high angles of attack

5. Enhanced Maneuverability of a Delta-Canard Combat Aircraft by Vortex Flow Control

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