Distributed Electric Propulsion Effects on Existing Aircraft Through Multidisciplinary Optimization-Reference-Cited by-同舟云学术

Distributed Electric Propulsion Effects on Existing Aircraft Through Multidisciplinary Optimization

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Moore Kevin R.¹,Ning Andrew¹

Affiliation:

1. Brigham Young University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1652

Reference26 articles.

1. Challenges of future aircraft propulsion: A review of distributed propulsion technology and its potential application for the all electric commercial aircraft

2. 4Yaros, S., Sexstone, M., Huebner, L., Lamar, J., McKinley., R., and Torres, A. “Synergistic airframe-propulsion interactions and integrations: a white paper prepared by the 1996-1997 Langley Aeronautics Technical Committee,” Tech. Rep. TM-1998-207644, NASA, 1998.

Cited by 12 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. A Review of Novel and Non-Conventional Propulsion Integrations for Next-Generation Aircraft;Designs;2024-02-20

2. Aerodynamic Performance Assessment of Distributed Electric Propulsion after the Wing Trailing Edge;Applied Sciences;2023-12-28

3. Two Aerodynamic Mid-Fidelity Approaches on a Distributed Propulsion Wing;Journal of Aircraft;2023-12-18

4. The effects of distributed electric propulsion on the aerodynamics of a regional aircraft wing;INCAS BULLETIN;2023-12-02

5. Aerodynamic and Structural Aspects of a Distributed Propulsion System for Commuter Airplane;Aerospace;2022-11-12