000 04861nam a2200481Ii 4500
001 9781315370613
003 FlBoTFG
005 20220711212215.0
006 m o d
007 cr
008 190122t20182016fluab ob 001 0 eng d
020 _a9781315370613 (e-book : PDF)
035 _a(OCoLC)960210301
040 _aFlBoTFG
_cFlBoTFG
_erda
041 1 _aeng
050 4 _aTL574
_b.A37
072 7 _aSCI
_x041000
_2bisacsh
072 7 _aTEC
_x009070
_2bisacsh
072 7 _aTQ
_2bicscc
082 0 4 _a629.132362
100 1 _aBhat, Rama B.,
_eauthor.
_914293
245 1 0 _aPrinciples of Aeroelasticity /
_cby Rama B. Bhat.
250 _aFirst edition.
264 1 _aBoca Raton, FL :
_bCRC Press,
_c[2018].
264 4 _c©2016.
300 _a1 online resource (185 pages) :
_b69 illustrations, text file, PDF
336 _atext
_2rdacontent
337 _acomputer
_2rdamedia
338 _aonline resource
_2rdacarrier
505 0 0 _tIntroductionElementary AerodynamicsGeneral ConceptsThe Joukowski Transformation for AirfoilsDimensional Analysis of Force Experienced by a Solid Body in a FlowStatic AeroelasticityIntroductionDetermination of Shear Center in a Thin-Walled SectionDivergence of a Lifting SurfaceIntroductionDivergence of a Typical Section with a Control SurfaceIntroductionControl Surface ReversalDynamic AeroelasticityIntroductionVibration TheoryDamped Single DOF SystemEnergy MethodSinusoidal ExcitationPeriodic ForceArbitrary ForceTwo DOF SystemEquations of Motion of a Two DOF Model of an Aircraft WingQuasi-Steady Aerodynamic TheoryCan Flutter Be Seen If Only Torsional Motion Is Considered?Dynamics of AirfoilRandom MotionOne-Dimensional Aeroelastic Model of AirfoilsIntroductionSimple Torsion of a BarGeneral Approximations for Aerodynamic TheoryEigenvalue and Eigenfunction ApproachesRolling of a Straight WingIntroductionDetermination of Aerodynamic Influence FunctionsFlutter of a Cantilever WingIntroductionSimple Bending of BeamsStability of the MotionApproximate Techniques of Modeling Continuous SystemsInfluence Coefficient MethodGalerkins MethodRayleigh-Ritz MethodFinite Element MethodAssembly of Finite ElementsFinite Element Representation of the Response and Flutter ProblemsElastic FoundationEigenfunctions and EigenvaluesNonairfoil Physical ProblemsDivergenceStall FlutterFlutter and Buffeting of BridgesAeroelasticity of Turbomachinery BladesNonlinear AeroelasticityGeneric Nonlinear Aeroelastic BehaviorOne Degree of Freedom Nonlinear System: DivergenceOne Degree of Freedom System: Dynamic EffectsTwo Degrees of Freedom System: Dynamic EffectsUnsteady AerodynamicsIntroductionTheodorsens Unsteady Thin-Airfoil TheoryFlutter Prediction via Assumed ModesReferences.
520 3 _aIntroductory Guide on the Design of Aerospace Structures. Developed from a course taught at Concordia University for more than 20 years, Principles of Aeroelasticity utilizes the author's extensive teaching experience to immerse undergraduate and first-year graduate students into this very specialized subject. Ideal for coursework or self-study, this detailed examination introduces the concepts of aeroelasticity, describes how aircraft lift structures behave when subjected to aerodynamic loads, and finds its application in aerospace, civil, and mechanical engineering. The book begins with a discussion on static behavior, and moves on to static instability and divergence, dynamic behavior leading up to flutter, and fluid structure interaction problems. It covers classical approaches based on low-order aerodynamic models and provides a rationale for adopting certain aeroelastic models. The author describes the formulation of discrete models as well as continuous structural models. He also provides approximate methods for solving divergence, flutter, response and stability of structures, and addresses non-aeroelastic problems in other areas that are similar to aeroelastic problems. Topics covered include: The fundamentals of vibration theory Vibration of single degree of freedom and two degrees of freedom systems Elasticity in the form of an idealized spring element Repetitive motion Flutter phenomenon Classical methods, Rayleigh-Ritz techniques, Galerkin's technique, influential coefficient methods, and finite element methods Unsteady aerodynamics, and more.
530 _aAlso available in print format.
650 0 _aAeroelasticity.
_96733
650 7 _aTECHNOLOGY & ENGINEERING / Mechanical.
_2bisacsh
_914294
650 7 _aAerodynamics.
_2bisacsh
_98123
650 7 _aStatics.
_2bisacsh
_95354
650 7 _aVibrations.
_2bisacsh
_914295
655 0 _aElectronic books.
_93294
710 2 _aTaylor and Francis.
_910719
776 0 8 _iPrint version:
_z9781498724722
856 4 0 _uhttps://www.taylorfrancis.com/books/9781315370613
_zClick here to view.
942 _cEBK
999 _c70667
_d70667