Flight Testing [electronic resource] : Analysis of the Spin Dynamics of a Single-Engine Low-Wing Aeroplane / by Steffen Haakon Schrader.

Por: Schrader, Steffen Haakon [author.]Colaborador(es): SpringerLink (Online service)Tipo de material: Texto

TextoEditor: Berlin, Heidelberg : Springer Berlin Heidelberg : Imprint: Springer Vieweg, 2023Edición: 1st ed. 2023Descripción: XI, 266 p. 188 illus., 145 illus. in color. online resourceTipo de contenido: text Tipo de medio: computer Tipo de portador: online resourceISBN: 9783662632185Tema(s): Aerospace engineering | Astronautics | Aerospace Technology and AstronauticsFormatos físicos adicionales: Printed edition:: Sin título; Printed edition:: Sin títuloClasificación CDD: 629.1 Clasificación LoC:TL1-4050Recursos en línea: Libro electrónico Texto

Contenidos:

Literature review -- Measurement system for spin test data acquisition -- Preparation of the aeroplane and the spin trials -- Spin description -- Mathematical spin test data analysis -- Flight test data comparison.

En: Springer Nature eBookResumen: As spinning is involved in around 60% of all aircraft accidents, this aerodynamic phenomenon is still not fully understood. This book contributes to a better understanding of the spin through investigating the spin regime for normal, utility and aerobatic aircraft, and to explain what happens to the aircraft in terms of the aerodynamics, flight mechanics and the aircraft stability. The approach used is to vary the main geometric parameters such as the center of gravity position and the aeroplane's mass across the flight envelope, and to investigate the subsequent effect on the main spin characteristic parameters. A conventional-geometry, single-engine low-wing aeroplane, has been instrumented with a proven digital flight measurement system and 27 spins have been systematically conducted inside and outside the certified flight envelope. The data collected include left and right wing α and β-angles, roll-pitch-yaw angles and corresponding rates, all control surface deflections, vertical speeds, altitude losses and the aeroplane's accelerations in all three directions. Such data have been statistically analysed and the pitch behaviour has been mathematically modelled. These results can be used to improve flight test programmes, aircraft design processes, flight training materials and hence contribute strongly to better flight safety.

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Existencias
Tipo de ítem	Biblioteca actual	Colección	Signatura	Copia número	Estado	Fecha de vencimiento	Código de barras
Libro Electrónico	Biblioteca Electrónica	Colección de Libros Electrónicos		1	No para préstamo

Acceso multiusuario

As spinning is involved in around 60% of all aircraft accidents, this aerodynamic phenomenon is still not fully understood. This book contributes to a better understanding of the spin through investigating the spin regime for normal, utility and aerobatic aircraft, and to explain what happens to the aircraft in terms of the aerodynamics, flight mechanics and the aircraft stability. The approach used is to vary the main geometric parameters such as the center of gravity position and the aeroplane's mass across the flight envelope, and to investigate the subsequent effect on the main spin characteristic parameters. A conventional-geometry, single-engine low-wing aeroplane, has been instrumented with a proven digital flight measurement system and 27 spins have been systematically conducted inside and outside the certified flight envelope. The data collected include left and right wing α and β-angles, roll-pitch-yaw angles and corresponding rates, all control surface deflections, vertical speeds, altitude losses and the aeroplane's accelerations in all three directions. Such data have been statistically analysed and the pitch behaviour has been mathematically modelled. These results can be used to improve flight test programmes, aircraft design processes, flight training materials and hence contribute strongly to better flight safety.

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