Estimating of Aerodynamic and Analysis of Aeroelasticity for Hypersonic Projectile

Article Preview

Abstract:

Dased on the analysis of characteristics of flow around slender body, this paper analyzes aerodynamic force and aeroelastic of slender body.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

978-981

Citation:

Online since:

November 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Xie Changchuan, Wu Zhigang,Yang Chao. Aeroela stic analysis of flexible large a spect ratio wing. Journal of Beijing University of Aeronautics and Astronautics, 2003:29(12)

Google Scholar

[2] Anderson John D, Jr. Fundamentals of Aerodynamics[M]. New York:: McGraw-Hill Book company, 1991.

Google Scholar

[3] Ma Songhui,Wu fuchengfu,Chenhuaimin. Study on Stability and Maneuverability of Flying Wing Aircraft.《{TTP}12298 Flight Dynamics》{TTP}12299 ,2006,24 (3) : 17221

Google Scholar

[4] Mou rangke,Yang yongnian. An Investigation of Airfoil Nonlinear Flutter Characteristics at Transonic Speed,《{TTP}12298 Chinese Journal of Applied Mechanics》{TTP}12299 ,VOL.18,SI,(2001)

Google Scholar

[5] H.W. Forsching. Principles of aeroelasticity. Translated by Shen Ke Yang.ShangHai: Shanghai Science and Technology Literature Publishing House. (1982)

Google Scholar

[6] H.W. Forsching. Principles of aeroelasticity. Translated by Shen Ke Yang.ShangHai: Shanghai Science and Technology Literature Publishing House. (1982)

Google Scholar

[7] Chen wenJun. Aeroelastic divergence analysis of projectile [R]. National Defense Report GF-A0017343G,1995.11

Google Scholar

[8] Li FengWei. Introduction of Air and Gas Dynamics[M]. Xi'aAn: Northwestern polytechnical university press, (2007)

Google Scholar