A nonlinear model for aircraft brake squeal analysis part II: Stability analysis and parametric studies

AIAA Dynamics Specialists Conference

Volumn , Issue , 1996, Pages 417-426

  Gordon, James T ^a   Liut, Steven Y ^a   Ozbek, M Akif ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BRAKES; DYNAMOMETERS; EIGENVALUES AND EIGENFUNCTIONS; FRICTION; FRICTION MATERIALS; LANDING GEAR (AIRCRAFT); NONLINEAR EQUATIONS; NONLINEAR SYSTEMS; TRIBOLOGY; VIBRATION ANALYSIS; WHEELS;

AIRCRAFT BRAKE SYSTEMS; CONSTANT-FRICTION COEFFICIENT; FRICTION COEFFICIENTS; NON-LINEAR DYNAMIC EQUATIONS; PERTURBATION EQUATION; STEADY-STATE OPERATING; TIME HISTORY RESPONSE; TORSIONAL STIFFNESS;

SYSTEM STABILITY;

EID: 84977134593     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1252     Document Type: Conference Paper

References (2)

1. S.Y. Liu, J.T. Gordon, and M.A. Ozbek. A nonlinear model for aircraft brake squeal analysis, part i: Model description and solution methodology. (Paper 96-1251 presented at the AIAA Dynamics Specialists Conference, April 1996).
2. Easy5x users guide. Boeing Computer Services Document BCS 20491-0530-R1, The Boeing Company, January 1993.