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Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations - A Generic Approach from Subsonic to Hypersonic Speeds (Hardcover, 1st ed. 2019)
Loot Price: R3,963
Discovery Miles 39 630
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Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations - A Generic Approach from Subsonic to Hypersonic Speeds (Hardcover, 1st ed. 2019)
Series: Springer Aerospace Technology
Expected to ship within 12 - 17 working days
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This 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?
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