Study of Ditching Characteristics of Transport Aircraft by Global Moving Mesh Method-Reference-Cited by-同舟云学术

Study of Ditching Characteristics of Transport Aircraft by Global Moving Mesh Method

Published:2015-09 Issue:5 Volume:52 Page:1550-1558
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Qu Qiulin¹,Hu Mingxuan¹,Guo Hao¹,Liu Peiqing¹,Agarwal Ramesh K.²

Affiliation:

1. Institute of Fluid Mechanics, Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China

2. Department of Mechanical Engineering and Materials Science, Washington University in St. Louis, St. Louis, Missouri 63130

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032993

Reference13 articles.

1. KarmanV. T. “The Impact of Seaplane Floats During Landing,” NACA TN-321, 1929.

2. FisherL. J.HoffmanE. L. “Model Ditching Investigation of the Douglas DC-4 and DC-6 Airplanes,” NACA RM-SL9K02A, 1949.

3. McBrideE. E.FisherL. J. “Experimental Investigation of the Effect of Rear-Fuselage Shape on Ditching Behavior,” NACA TN-2929, 1953.

4. ThompsonW. C. “Model Ditching Investigation of the Boeing 707 Jet Transport,” NACA RM-SL55K08, 1955.

5. ThompsonW. C. “Rough-Water Ditching Investigation of a Model of a Jet Transport with the Landing Gear Extended and with Various Ditching Aids,” NASA TN-D-101, 1959.

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