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001 978-3-030-16856-8
003 DE-He213
005 20220801215311.0
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008 190723s2019 sz | s |||| 0|eng d
020 _a9783030168568
_9978-3-030-16856-8
024 7 _a10.1007/978-3-030-16856-8
_2doi
050 4 _aTL1-4050
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
072 7 _aTRP
_2thema
072 7 _aTTDS
_2thema
082 0 4 _a629.1
_223
100 1 _aChudoba, Bernd.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_943534
245 1 0 _aStability and Control of Conventional and Unconventional Aerospace Vehicle Configurations
_h[electronic resource] :
_bA Generic Approach from Subsonic to Hypersonic Speeds /
_cby Bernd Chudoba.
250 _a1st ed. 2019.
264 1 _aCham :
_bSpringer International Publishing :
_bImprint: Springer,
_c2019.
300 _aXXXIV, 392 p.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSpringer Aerospace Technology,
_x1869-1749
505 0 _aIntroduction and Objectives -- Generic Aircraft Design – Knowledge Utilization -- Assessment of the Aircraft Conceptual Design Process -- Generic Characterisation of Aircraft – Parameter Reduction Process -- ‘AeroMech’ – Conception of a Generic Stability and Control Methodology -- AeroMech Feasibility -- Conclusions -- Appendices.
520 _aThis book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis. The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific method itself is derived throughout the second half of the book. This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a ‘configuration stability & control’ methodology module for an advanced multi-disciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations?
650 0 _aAerospace engineering.
_96033
650 0 _aAstronautics.
_943535
650 0 _aMultibody systems.
_96018
650 0 _aVibration.
_96645
650 0 _aMechanics, Applied.
_93253
650 0 _aEngineering design.
_93802
650 1 4 _aAerospace Technology and Astronautics.
_943536
650 2 4 _aMultibody Systems and Mechanical Vibrations.
_932157
650 2 4 _aEngineering Design.
_93802
710 2 _aSpringerLink (Online service)
_943537
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783030168551
776 0 8 _iPrinted edition:
_z9783030168575
776 0 8 _iPrinted edition:
_z9783030168582
830 0 _aSpringer Aerospace Technology,
_x1869-1749
_943538
856 4 0 _uhttps://doi.org/10.1007/978-3-030-16856-8
912 _aZDB-2-ENG
912 _aZDB-2-SXE
942 _cEBK
999 _c77338
_d77338