Simulation of Arresting Dynamics on the Carrier

Article Preview

Abstract:

The article puts forward a method for calculating the arresting force of carrier aircraft in the case the aircraft meets the cable off-center and the aircraft motion is unsymmetrical. The condition under which the hook will or will not slip on the cable is considered. Based on a great deal of numerical results, the article analyzed the impact of unsymmetrical motion and off-center on landing dynamics of carrier aircraft.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 199-200)

Pages:

156-160

Citation:

Online since:

February 2011

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2011 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Jones Lyle W. Development of curves for estimating aircraft arresting hook loads [R]. AFFT C-TIM-81-3. (1982).

Google Scholar

[2] HQ AFCESA/CEXR. Guide to Mobile Aircraft Arresting System Installation. Air Force Handbook. 2000, 8: 10~222.

Google Scholar

[3] Major John O. Jordan. Marine Tac Air and the STOVL Penalty: Myth or Menace (Master of Military Studies), United Stated Marine Corps. Command and Staff College, Marine Corps University. (2000).

Google Scholar

[4] Air Force Installations and Facilities. Planning Guide for Installation of Ultra-High-Molecular-Weight(UHMW) Polyethylene Panels under Aircraft Arresting System Cables(CONUS Installations), (1995).

DOI: 10.21236/ada508608

Google Scholar

[5] Qiansheng Wang. Critical Technologies in Carrier-Based Aircraft Design and Development. AIRCRAFT DESIGN [J], 2005, 2: 6~10 (in Chinese).

Google Scholar

[6] Department of Defense Handbook. MIL-HDBK-2066 [S]. (1999).

Google Scholar

[7] Zhenping Fang, Wanchun Chen, Shuguang Zhang. The dynamics of aircraft [M]. Beijing: Beijing University of Aeronautics andAstronautics press, 2005: 22~25 (in Chinese).

Google Scholar