001461256 000__ 03802cam\a2200589\i\4500
001461256 001__ 1461256
001461256 003__ OCoLC
001461256 005__ 20230503003343.0
001461256 006__ m\\\\\o\\d\\\\\\\\
001461256 007__ cr\un\nnnunnun
001461256 008__ 230317s2023\\\\gw\a\\\\ob\\\\000\0\eng\d
001461256 019__ $$a1372399561
001461256 020__ $$a9783662632185$$q(electronic bk.)
001461256 020__ $$a3662632187$$q(electronic bk.)
001461256 020__ $$z9783662632178
001461256 020__ $$z3662632179
001461256 0247_ $$a10.1007/978-3-662-63218-5$$2doi
001461256 035__ $$aSP(OCoLC)1372321690
001461256 040__ $$aYDX$$beng$$erda$$epn$$cYDX$$dGW5XE$$dEBLCP$$dOCLCF
001461256 049__ $$aISEA
001461256 050_4 $$aTL574.S6
001461256 08204 $$a629.132$$223/eng/20230317
001461256 1001_ $$aSchrader, Steffen Haakon,$$eauthor.
001461256 24510 $$aFlight testing :$$banalysis of the spin dynamics of a single-engine low-wing aeroplane /$$cSteffen Haakon Schrader.
001461256 264_1 $$aBerlin :$$bSpringer Vieweg,$$c[2023]
001461256 264_4 $$c©2023
001461256 300__ $$a1 online resource (xi, 266 pages) :$$billustrations (chiefly color)
001461256 336__ $$atext$$btxt$$2rdacontent
001461256 337__ $$acomputer$$bc$$2rdamedia
001461256 338__ $$aonline resource$$bcr$$2rdacarrier
001461256 504__ $$aIncludes bibliographical references.
001461256 5050_ $$aLiterature 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.
001461256 506__ $$aAccess limited to authorized users.
001461256 520__ $$aAs 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 aeroplanes 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 and -angles, roll-pitch-yaw angles and corresponding rates, all control surface deflections, vertical speeds, altitude losses and the aeroplanes 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.
001461256 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed March 17, 2023).
001461256 650_0 $$aSpin (Aerodynamics)
001461256 655_0 $$aElectronic books.
001461256 77608 $$iPrint version: $$z3662632179$$z9783662632178$$w(OCoLC)1240771982
001461256 852__ $$bebk
001461256 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-3-662-63218-5$$zOnline Access$$91397441.1
001461256 909CO $$ooai:library.usi.edu:1461256$$pGLOBAL_SET
001461256 980__ $$aBIB
001461256 980__ $$aEBOOK
001461256 982__ $$aEbook
001461256 983__ $$aOnline
001461256 994__ $$a92$$bISE