Hypersonic vehicle control concept using an active shock bump technique-Reference-Cited by-同舟云学术

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Hypersonic vehicle control concept using an active shock bump technique

Published:2018-09-15 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
language:
Short-container-title:

Author:

Bliamis Christos¹,Panagiotou Pericles¹,Yakinthos Kyros¹

Affiliation:

1. Aristotle University of Thessaloniki

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5376

Reference17 articles.

1. Anderson,J.D.,Hypersonicandhigh-temperaturegasdynamics,2nded.,AmericanInstituteofAeronauticsandAstronautics, Reston,Va,2006.

2. Raymer,D.P.,AircraftDesign:AConceptualApproach,5thed.,AmericanInstituteofAeronauticsandAstronautics,Reston, VA,2012.

3. Airplane Stability and Control, Second Edition

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. Path-Following Control for Thrust-Vectored Hypersonic Aircraft;Energies;2023-03-06

2. A novel technique for hypersonic vehicle control;MATEC Web of Conferences;2019

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