THE MODAL FEATURES OF VIBRATION SYSTEMS WITH WEAKLY-VISCOELASTIC MATERIAL STRUCTURES

DYNAMIC SHAKEDOWN ANALYSIS OF WORK-HARDENING STRUCTURES UNDER CYCLING LOADS Northwestern Polytechnical University

THE APPLICATION OF THE HIERACHICAL FINITE ELEMENT TECHNIQUE IN THE TIME DOMAIN

NONLINEAR DYNAMIC ANALYSIS OF LAMINATED COMPOSITE STRUCTURE UNDER IMPACT LOADS

TRANSFER MATRIX METHOD ALLOWING FOR VARIATION OF SECTION PARAMETERS AND CONTINUITY OF MASS IN ELEMENT

AIR SURVEYING AND DATA ANALYSIS FOR DYNAMIC RESPONSE OF MISSILES AT SWEPT-BACK WING TIP

MODAL ANALYSIS FOR FIBRE-CARBON COMPOSITE PARTS OF AN AIRPLANE

THE NONLINEAR DYNAMIC RESPONSE ANALYSIS OF THE FRONT WINDSHIELD OF Y12 UNDER“BIRD-IMPACT”LOADS

A NUMERICAL STUDY ON COUPLED DYNAMIC ANALYSIS OF LIQUID CONTAINERS

APPLICATION OF ACOUSTICALLY TREATED HONEYCOMB SANDWICH PANELS IN NOISE CONTROL OF AIRCRAFT CABIN

NUMERICAL ANALYSIS OF SOLID-FLUID INTERACTIVE VIBRATION OF AN AIRCRAFT INTEGRAL TANK

CALCULATION AND EXPERIMENTAL STUDY ON SONIC FATIGUE LIFE OF AIRCRAFT STRUCTURAL PANELS

VIBRATION OF CRACKED PLATE

FURTHER RESEARCH ON MECHANICAL MODEL FOR'GROUND RESONANCE"OF HELICOPTERS

VIBRATION PROBLEMS IN AN AIRCRAFT DESIGN

SIMILARITIES AND DIFFERENCES BETWEEN ENVIROMMENT TESTS AND RELIABILITY TESTS IN VIEW OF VIBRATION

APPLICATION OF IDENTIFICATION METHOD OF MODAL PARAMETER TO FLIGHT FLUTTER TEST

INTEGRATION OF VIBRATION TEST AND FLUTTER ANALYSIS——A BRIEF INTRODUCTION TO "A REAL-TIME FLUTTER ANALYSIS SYSTEM"

TRANSONIC FLUTTER ANALYSIS OF 2-D AIRFOILS WITH 2 DEGREES OF FREEDOM

IDENTIFICATION OF NACELLE MODES FROM AIRPLANE GVT RESULTS

A STUDY ON SONIC LOAD OF THE VERTICAL TAIL OF F-7 AIRCRAFT

FLEXURE VIBRATION TEST METHOD OF AVIATION TUBE

STUDY ON VIBRATION AND SHOCK TEST PARAMETER FOR AVIATION ROCKET LAUNCHERS

A NUMERICAL METHOD FOR SIMULATING DROP TEST OF LANDING GEARS

PREDICTION OF TEST SPECTRUM FOR GUNFIRE VIBRATION