Reseña. Aeroplane construction and strength analysis
Este libro es el número dos de la Colección Facultad de Ingeniería, que ya tiene algunos títulos en prensa y otros en preparación. El libro tiene sus orígenes en un texto de lecturas para los estudiantes del Instituto de Aviación de la Universidad Técnica de Riga. El autor escribió en ruso, pero fue vertido al inglés y revisado por el ingeniero aeronáutico Guido Fuentes en la Facultad de Ingeniera de la Universidad de San Buenaventura, Bogotá D.C.
Esta obra constituye un material de enorme interés e importancia para el área de la ingeniera aeronáutica, puesto que no existen escritos similares en inglés ni en otros idiomas.
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Contenido. Aeroplane construction and strength analysis
Presentation
Introduction
CHAPTER
AEROPLANE DESIGN AND DEVELOPMENT
Configuration development. Initial specification.
Impact of civil airworthiness requirements and operational rules.
Take-off mass.
EXTERNAL FLIGHT LOADS
D`Alembert`s principle, load factor.
Experimental investigation of load factor.
The airplane in a vertical plane maneuver.
The airplane in a vertical plane maneuver.
The airplane in a gust.
Flight condition influence.
ATM. Requirements to the strength under loads.
Definitions of ATM.
Design airspeed.
ATM. Requirements to strength and deformation.
Design gust loads.
Flight maneuvering loads.
DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE
Main components of fatigue failure problem of airplane structure. Main stages of its solution.
Typical loading spectrum expected in service.
Two models of turbulence.
Fatigue characteristics.
Linear rule of summing of fatigue damage (Miner`s rule)
Full cycle method.
Safe-life calculation
Damage tolerance.
Design a damage tolerant structure.
WING
Requirements.
Wing loads.
Internal force factors in cross sections of a wing.
Structure and structural model of a wing.
Types of wing structure.
Strength analysis of a wing.
Strength and structured of wing details.
Specific features of strength analysis of root cross-section.
FLIGHT CONTROL DEVICES
Ailerons and spoilers.
Aileron strength analysis.
Empennage.
Empennage loads.
Specific features of structure and strength analysis of the empennage.
Reduction of control forces.
HIGH-LIFT DEVICES
Trailing-edge flaps.
Leading-edge high-lift device.
Horizontal acceleration and deceleration control means.
Structure and strength analysis of flaps.