Roll reversal phenomenon control in flight vehicles-Reference-Cited by-同舟云学术

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Roll reversal phenomenon control in flight vehicles

Published:2018-08 Issue: Volume:79 Page:413-425
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Mirzaei Mojtaba

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Simulation validation of static and forced motion flow physics of a canard configured TransCruiser;Ghoreyshi;Aerosp. Sci. Technol.,2016

2. Studies of vortex interference associated with missile configurations;Lesieutre,2014

3. Numerical investigation of canard-controlled missile with planar and grid fins;De Spirito;J. Spacecr. Rockets,2003

4. The effect of tail fin parameters on the induced roll of a canard-controlled missile;McDaniel,2010

5. Experimental study of tail-span effects on a canard-controlled missile;Blair;J. Spacecr. Rockets,1993

Cited by 2 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. Numerical investigation of aerodynamic characteristics of free-spinning tail projectile with canards roll control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-08-27

2. The numerical investigation on the rolling decoupling of a canard-controlled missile using the jet control system;Engineering Applications of Computational Fluid Mechanics;2020-01-01

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