Wake Impact Alleviation Control Based on Wake Identification-Reference-Cited by-同舟云学术

Wake Impact Alleviation Control Based on Wake Identification

Published:2015-11 Issue:6 Volume:52 Page:2077-2089
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Ehlers Jana¹,Fischenberg Dietrich¹,Niedermeier Dominik¹

Affiliation:

1. Institute of Flight Systems, Department Flight Dynamics and Simulation, DLR, German Aerospace Center, 38108 Braunschweig, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033157

Reference25 articles.

1. “In-Flight Separation of Vertical Stabilizer American Airlines Flight 587 Airbus Industrie A300-605R, N14053 Belle Harbor, New York November 12, 2001,” National Transportation Safety Board Aircraft Accident Rept. NTSB/AAR-04/04, Washington, D.C. 2004.

2. Evaluation of flight spoilers for vortex alleviation

3. Experimental study of the instability of unequal-strength counter-rotating vortex pairs

4. Wake Vortex Alleviation Flow Field Studies

5. Active Control of a Wing Tip Vortex

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