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Flight testing = analysis of the spi...

Schrader, Steffen Haakon.

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Flight testing = analysis of the spin dynamics of a single-engine low-wing aeroplane /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Flight testing/ by Steffen Haakon Schrader.
其他題名:	analysis of the spin dynamics of a single-engine low-wing aeroplane /
作者:	Schrader, Steffen Haakon.
出版者:	Berlin, Heidelberg :Springer Berlin Heidelberg : : 2023.,
面頁冊數:	xi, 266 p. :ill. (chiefly col.), digital ;24 cm.
內容註:	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.
Contained By:	Springer Nature eBook
標題:	Spin (Aerodynamics) -
電子資源:	https://doi.org/10.1007/978-3-662-63218-5
ISBN:	9783662632185

Flight testing = analysis of the spin dynamics of a single-engine low-wing aeroplane /
Schrader, Steffen Haakon.

Flight testinganalysis of the spin dynamics of a single-engine low-wing aeroplane /[electronic resource] :by Steffen Haakon Schrader. - Berlin, Heidelberg :Springer Berlin Heidelberg :2023. - xi, 266 p. :ill. (chiefly col.), digital ;24 cm.

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.

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.

ISBN: 9783662632185

Standard No.: 10.1007/978-3-662-63218-5doiSubjects--Topical Terms:

3631507
Spin (Aerodynamics)

LC Class. No.: TL574.S6

Dewey Class. No.: 629.132

Flight testing = analysis of the spin dynamics of a single-engine low-wing aeroplane /
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520 $a 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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