2017
DOI: 10.1115/1.4036808
|View full text |Cite
|
Sign up to set email alerts
|

Actuator Design and Flight Testing of an Active Microspoiler-Equipped Projectile

Abstract: Actively controlled gun-launched projectiles require a means of modifying the projectile flight trajectory. While numerous potential mechanisms exist, microspoiler devices have been shown to be a promising control actuator for fin-stabilized projectiles in supersonic flight. These devices induce a trim force and moment generated by the boundary layer–shock interaction between the projectile body, rear stabilizing fins, and microspoilers. Previous investigations of microspoiler mechanisms have established estim… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2019
2019
2022
2022

Publication Types

Select...
2
1

Relationship

0
3

Authors

Journals

citations
Cited by 3 publications
(1 citation statement)
references
References 26 publications
0
1
0
Order By: Relevance
“…Numerous research institutes have proposed kinds of FE actuator configurations, of which there are two main types: one adopts the traditional mechanism and simple physics theory for design, while the other applies new intelligent materials or new structures. Kim et al [6] proposed an FE The associate editor coordinating the review of this manuscript and approving it for publication was Gursel Alici.…”
Section: Introductionmentioning
confidence: 99%
“…Numerous research institutes have proposed kinds of FE actuator configurations, of which there are two main types: one adopts the traditional mechanism and simple physics theory for design, while the other applies new intelligent materials or new structures. Kim et al [6] proposed an FE The associate editor coordinating the review of this manuscript and approving it for publication was Gursel Alici.…”
Section: Introductionmentioning
confidence: 99%