Ultrasonic Health Monitoring of Thermoplastic Composite Aircraft Primary Structures

Multi-level repair decision-making process for composite structures

Residual thermal stresses around bonded fibre metal laminate repair patches on an aircraft fuselage

A MATLAB program to study gust loading on a simple aircraft model

Aircraft corrosion and fatigue damage assessment (USAF ASIP Publication)

Aircraft corrosion and fatigue damage assessment

The use of load enhancement factors in the certification of composite aircraft structures

European approaches in standard spectrum development

Damage tolerance of stiffened-skin structures: prediction and experimental verification

An introductory course on aircraft loading

Residual strength of (0, ±45)s and (±45, 0)s carbon/epoxy laminates

Aluminium alloys for advanced structural applications in transport aircraft

The requirement of damage tolerance: An analysis of damage tolerance requirements with specific reference to MIL-A-83444

Residual strength data of riveted panels with different stiffener configurations

User's manual of ARREST, a computer routine for prediction of residual strength of cracked stiffened panels

Calculation of vibration modes and resonance frequencies of the Northrop NF-5