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

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

Author:

Deiler Christoph¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

Reference29 articles.

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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