Nonlinear model for aircraft brake squeal analysis: Stability analysis and parametric studies

Journal of Aircraft

Volumn 35, Issue 4, 1998, Pages 631-636

  Gordon, James T ^a,b,c   Liu, Steven Y ^a,b   Akif Ozbek M ^a,b,c  

^a BOEING COMPANY   (United States)

^b Structures Vibration Technology   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT PARTS AND EQUIPMENT; BRAKES; DAMPING; DYNAMOMETERS; EIGENVALUES AND EIGENFUNCTIONS; FRICTION; NONLINEAR EQUATIONS; PERTURBATION TECHNIQUES; PRESSURE EFFECTS; STIFFNESS; VIBRATIONS (MECHANICAL);

AIRCRAFT BRAKE SQUEAL ANALYSIS; BRAKE FRICTION COEFFICIENT; NONLINEAR DYNAMIC EQUATION; NONLINEAR MODEL; STABILITY ANALYSIS; TORSIONAL STIFFNESS;

MATHEMATICAL MODELS;

EID: 0032118513     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2347     Document Type: Article

References (2)

1. Liu, S. Y., Gondon, J. T., and Özbek, M. A., "Nonlinear Model for Aircraft Brake-Squeal Analysis: Model Description and Solution Methodology," Journal of Aircraft,Vol. 35, No. 4, 1998, pp. 623-630.
2. Easy5x Users Guide, Boeing Computer Services Document BCS 20491-0530-R1, The Boeing Co., Seattle, WA, Jan. 1993.