Evaluation of flight spoilers for vortex alleviation-Reference-Cited by-同舟云学术

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Evaluation of flight spoilers for vortex alleviation

Published:1977-08 Issue:8 Volume:14 Page:823-825
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Croom Delwin R.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.44620

Reference9 articles.

1. Yff, J. "Analysis of Dynamic Aircraft Landing Loads and a Proposal for Rational Design Landing Load Requirements," Ph.D. Dissertation,June27,1972, Technische Hogeschool, Delft, Netherlands.

2. 3Milwitzky, B. and Cook, F. C. "Analysis of Landing Gear Behavior," NACA Report 1154, 1953.

Cited by 3 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. Near field evolution of wingtip vortices under synthetic-jet based control;Aerospace Science and Technology;2024-05

2. Wake Impact Alleviation Control Based on Wake Identification;Journal of Aircraft;2015-11

3. Novel Aerodynamic Device for Wake Vortex Alleviation;AIAA Journal;2007-09

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