Structural Design Exploration of an Electric Powered Multi-propulsor Wing Configuration-Reference-Cited by-同舟云学术

Structural Design Exploration of an Electric Powered Multi-propulsor Wing Configuration

Published:2017-01-05 Issue: Volume: Page:
ISSN:
Container-title:58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Moore James¹,Cutright Stephen¹,Viken Jeffrey K.¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0203

Reference14 articles.

1. Aeroelastic Tailoring of the NASA Common Research Model via Novel Material and Structural Configurations

2. Drag Reduction Through Distributed Electric Propulsion

3. Anon. "Minimizing the Hazards from Propeller Blade and Hub Failures," FAA Advisory Circular AC-25.905, http://www.faa.gov/regulations_policies/advisory_circulars/index.cfm/go/document.information/documentID/22 675, Washington, DC, September 27, 2000.

4. Anon. "Aeroelastic Stability Substantiation of Transport Category Airplanes," FAA Advisory Circular AC25.629-1A. http://www.faa.gov/regulations_policies/advisory_circulars/index.cfm/go/document.information/documentID/22 660, Washington, DC, July 23, 1998.

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. Fast Vibration Reduction Optimization Approach for Complex Thin-Walled Shells Accelerated by Global Proper Orthogonal Decomposition Reduced-Order Model;Applied Sciences;2022-12-29

2. Distributed pod wing modeling and aeroelastic analysis;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2022-10

3. Structural Analysis and Performance-Based Validation of a Composite Wing Spar;AIAA Scitech 2019 Forum;2019-01-06

4. Status Report on Aeroelasticity in the Vehicle Development for X-57 Maxwell;2018 Applied Aerodynamics Conference;2018-06-24