Closed-Loop Missile Yaw Control via Manipulation of Forebody Flow Asymmetrics-Reference-Cited by-同舟云学术

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Closed-Loop Missile Yaw Control via Manipulation of Forebody Flow Asymmetrics

Published:2004-05 Issue:3 Volume:41 Page:436-443
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Patel Mehul P.¹,Tilmann Carl P.²,Ng T. Terry³

Affiliation:

1. Orbital Research Inc., Cleveland, Ohio 44143

2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

3. University of Toledo, Toledo, Ohio 43606

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.10701

Reference32 articles.

1. Unsteady flow separation on slender bodies at high angles of attack

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1. Investigation of periodic characteristics of perturbed flow over a slender body;Heliyon;2023-05

2. Wake topology and dynamics over a slender body at a high incidence and their relation to structural loading;Physics of Fluids;2020-05-01

3. Feedback Flow Control: A Heuristic Approach;AIAA Journal;2018-10

4. CFD Simulations of a Finned Projectile with Microflaps for Flow Control;International Journal of Aerospace Engineering;2017

5. CFD Study on a Pitching Missile with Respect to Reduce the Phantom Yaw Effect;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2016

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