Aircraft Flight Dynamics with a Non-Inertial CFD Code-Reference-Cited by-同舟云学术

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Aircraft Flight Dynamics with a Non-Inertial CFD Code

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

O'Neill Charles¹,Arena Andrew¹

Affiliation:

1. Oklahoma State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-230

Reference16 articles.

1. Development of a finite element aeroelastic analysis capability

2. CFD-based Aeroservoelastic Analysis with Hyper-X Applications

3. 3Cowan, T. J., Finite Element CFD Analysis of Super-Maneuvering and Spinning Structures, Ph.D. thesis,Oklahoma State University, Stillwater, OK, August 2003.

4. Review of Attitude Representations Used for Aircraft Kinematics

Cited by 4 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. Determination and analysis of roll and yaw rotary derivatives of wig vehicle using numerical simulation;Aerospace Systems;2022-11-28

2. Numerical simulations of the flow around a square pitching panel;Journal of Fluids and Structures;2018-01

3. Propulsion Models Implemented in Finite Element CFD;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

4. Modeling Hypersonic Propulsion Using Finite Element CFD;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

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