Test and Simulation of Horizontal Tail Leading Edge Impacted by Bird-Reference-Cited by-同舟云学术

Test and Simulation of Horizontal Tail Leading Edge Impacted by Bird

Published:2022-09 Issue:5 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Jun¹,Zhang Chunyang²,Wu Zhibin³,Zhang Zhengli³

Affiliation:

1. Associate Professor, Dept. of Aeronautical Structure Engineering, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China (corresponding author).

2. Postgraduate, Dept. of Aeronautical Structure Engineering, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

3. Engineer, Commercial Aircraft Corporation of China, Ltd., 25 Zhangyang Rd., Shanghai 200120, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001454

Reference23 articles.

1. Characterization of real and substitute birds through experimental and numerical analysis of momentum, average impact force and residual energy in bird strike on three rigid targets: A flat plate, a wedge and a splitter

2. Development and validation of a set-up to measure the transferred multi-axial impact momentum of a bird strike on a booster vane

3. Numerical and experimental investigation of the shock and steady state pressures in the bird material during bird strike

4. Reprint of: The particle finite element method for the numerical simulation of bird strike

5. Chary, C. 2015. “Development and validation of a bird strike protection system for an enhanced adaptive droop nose.” In Smart intelligent aircraft structures, 71–83. Cham, Switzerland: Springer.

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