Effect of Initial Pitching Angle on Helicopter Ditching Characteristics Using Smoothed-Particle-Hydrodynamics Method-Reference-Cited by-同舟云学术

Effect of Initial Pitching Angle on Helicopter Ditching Characteristics Using Smoothed-Particle-Hydrodynamics Method

Published:2021-01 Issue:1 Volume:58 Page:167-181
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Xiao Tianhang¹,Lu Zhaoyan¹,Deng Shuanghou¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, Jiangsu, People’s Republic of China

Funder

Jiangsu Innovation Program for Graduate Education

Rotor Aerodynamic Key Laboratory

National Natural Science Foundation of China

China Scholarship Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference27 articles.

1. TosoN. R. S. “Contribution to the Modelling and Simulation of Aircraft Structures Impacting on Water,” Ph.D. Thesis, Univ. of Stuttgart, Stuttgart, Germany, 2009. 10.18419/opus-3823

2. From aerospace to offshore: Bridging the numerical simulation gaps–Simulation advancements for fluid structure interaction problems

3. Analytical method for the ditching analysis of an airborne vehicle

4. ReinhardM. V. “Free Elastic Plate Impact into Water,” Ph.D. Thesis, Univ. of East Anglia, Norwich, England, U.K. 2013.

5. FisherL. J.HoffmanE. L. “Model Ditching Investigation of the Douglas DC-4 and DC-6 Airplanes,” NACA RM-SL9 K02A, 1950.

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