Aerodynamic Modeling, System Identification, and Analysis of Iced Aircraft Configurations-Reference-Cited by-同舟云学术

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Aerodynamic Modeling, System Identification, and Analysis of Iced Aircraft Configurations

Published:2018-01 Issue:1 Volume:55 Page:145-161
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Deiler Christoph¹

Affiliation:

1. DLR, German Aerospace Center, 38108 Braunschweig, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034390

Reference29 articles.

1. A Study of U.S. Inflight Icing Accidents and Incidents, 1978 to 2002

2. “Bundesstelle für Flugunfalluntersuchung,” Final Rept. 5X011-0/98, Braunschweig, Germany, April 2001.

3. National Transportation Safety Board, Aircraft Accident Rept. NTSB/AAR-96/01, DCA95MA001, Washington, D.C. July 1996.

4. GrayV. H. “Prediction of Aerodynamic Penalties Caused by Ice Formations on Various Airfoils,” NASA, TN D-2166, Feb. 1964.

5. “Ice Accretion Simulation,” AGARD, Fluid Dynamics Panel Working Group 20, Rept. 344, Neuilly-sur-Seine, France, Dec. 1997.

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2. Retrospective and Recent Examples of Aircraft and Rotorcraft System Identification at DLR;Journal of Aircraft;2023-09

3. System Identification-informed Transparent and Explainable Machine Learning with Application to Power Consumption Forecasting;2023 3rd International Conference on Electrical, Computer, Communications and Mechatronics Engineering (ICECCME);2023-07-19

4. System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data;Journal of Aircraft;2023-07

5. Unstable tilt-rotor maximum likelihood wavelet-based identification from flight test data;Aircraft Engineering and Aerospace Technology;2023-06-12

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