Vibroacoustic Tailoring of a Rod-Stiffened Composite Fuselage Panel with Multidisciplinary Considerations-Reference-Cited by-同舟云学术

Vibroacoustic Tailoring of a Rod-Stiffened Composite Fuselage Panel with Multidisciplinary Considerations

Published:2015-03 Issue:2 Volume:52 Page:692-702
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Allen Albert R.¹,Przekop Adam¹

Affiliation:

1. Structural Acoustics Branch, NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033071

Reference22 articles.

1. Airframe Development for the Hybrid Wing Body Aircraft

2. VelickiA. “Damage Arresting Composites for Shaped Vehicles—Phase 1 Final Report,” NASA CR-15932, 2009.

3. VelickiA.YovanofN.BarajaJ.LintonK.LiV.HawleyA.ThrashP.DeCouxS.PickellR. “Damage Arresting Composites for Shaped Vehicles—Phase 2 Final Report,” NASA CR-216880, 2011.

4. LintonK. A.VelickiA.HoffmanK.ThrashP.PickellR.TurleyR. “PRSEUS Panel Fabrication Final Report,” NASA CR-2014-218149, 2014.

5. Nonlinear Finite Element Analysis of a Composite Non-Cylindrical Pressurized Aircraft Fuselage Structure

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Thermomechanical Collaborative Design and Experimental Verification of a Sandwich Structure with a Polyimide Foam Core;Journal of Aircraft;2024-06-27

2. Vibroacoustic studies on structurally optimized Pareto designs of curved composite stiffened panel;AIAA SCITECH 2024 Forum;2024-01-04

3. 基于响应面分析的碳纤维复合材料基体激光除漆工艺优化;Chinese Journal of Lasers;2023

4. Experimental Research on the Stability behavior of Composite Curved Stiffened Fuselage Panel under Four-Point-Bending load;IOP Conference Series: Materials Science and Engineering;2019-07-01