A Modern Course in Aeroelasticity: Solid Mechanics and Its Applications, cartea 32
Editat de E.H. Dowell, Edward F. Crawley, Howard C. Curtiss Jr., David A. Peters, Robert H. Scanlan, Fernando Sistoen Limba Engleză Paperback – 30 iun 1995
The authors are drawn from a range of fields including aerospace engineering, civil engineering, mechanical engineering, rotorcraft and turbomachinery. Each author is a leading expert in the subject of his chapter and has many years of experience in consulting, research and teaching.
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Specificații
ISBN-13: 9780792327899
ISBN-10: 0792327896
Pagini: 704
Ilustrații: XXIII, 704 p.
Dimensiuni: 160 x 240 x 37 mm
Greutate: 1.01 kg
Ediția:Softcover reprint of the original 3rd ed. 1995
Editura: SPRINGER NETHERLANDS
Colecția Springer
Seria Solid Mechanics and Its Applications
Locul publicării:Dordrecht, Netherlands
ISBN-10: 0792327896
Pagini: 704
Ilustrații: XXIII, 704 p.
Dimensiuni: 160 x 240 x 37 mm
Greutate: 1.01 kg
Ediția:Softcover reprint of the original 3rd ed. 1995
Editura: SPRINGER NETHERLANDS
Colecția Springer
Seria Solid Mechanics and Its Applications
Locul publicării:Dordrecht, Netherlands
Public țintă
ResearchCuprins
2. Static aeroelasticity.- 2.1 Typical section model of an airfoil.- 2.2 One dimensional aeroelastic model of airfoils.- 2.3 Rolling of a straight wing.- 2.4 Two dimensional aeroelastic model of lifting surfaces.- 2.5 Nonairfoil physical problems.- 2.6 Sweptwing divergence.- 3. Dynamic aeroelasticity.- 3.1 Hamilton’s principle.- 3.2 Lagrange’s equations.- 3.3 Dynamics of the typical section model of an airfoil.- 3.4 Aerodynamic forces for airfoils—an introduction and summary.- 3.5 Solutions to the aeroelastic equations of motion.- 3.6 Representative results and computational considerations.- 3.7 Generalized equations of motion for complex structures.- 3.8 Nonairfoil physical problems.- 4. Nonsteady aerodynamics of lifting and non-lifting surfaces.- 4.1 Basic fluid dynamic equations.- 4.2 Supersonic flow.- 4.3 Subsonic flow.- 4.4 Representative numerical results.- 4.5 Transonic flow.- 5. Stall flutter.- 5.1 Background.- 5.2 Analytical formulation.- 5.3 Stability and aerodynamic work.- 5.4 Bending stall flutter.- 5.5 Nonlinear mechanics description.- 5.6 Torsional stall flutter.- 5.7 General comments.- 5.8 Reduced order models.- 5.9 Computational stalled flow.- 6. Aeroelastic problems of civil engineering structures.- 6.1 Vortex shedding.- 6.2 Galloping.- 6.3 Divergence.- 6.4 Flutter and buffeting.- 7. Aeroelastic response of rotorcraft.- 7.1 Blade dynamics.- 7.2 Stall flutter.- 7.3 Rotor-body coupling.- 7.4 Unsteady aerodynamics.- 8. Aeroelasticity in turbomachines.- 8.1 Aeroelastic environment in turbomachines.- 8.2 The compressor performance map.- 8.3 Blade mode shapes and materials of construction.- 8.4 Nonsteady potential flow in cascades.- 8.5 Compressible flow.- 8.6 Periodically stalled flow in turbomachines.- 8.7 Stall flutter in turbomachines.- 8.8 Chokingflutter.- 8.9 Aeroelastic eigenvalues.- 8.10 Recent trends.- 9. Unsteady transonic aerodynamics and aeroelasticity.- Summary.- Nomenclature.- 9.1 Introduction.- 9.2 Linear / nonlinear behavior in unsteady transonic aerodynamics.- 9.3 Viable alternative solution procedures to finite difference methods.- 9.4 Nonuniqueness.- 9.5 Effective, efficient computational approaches for determining aeroelastic response.- 9.6 Nonlinear flutter analysis in the frequency domain.- 9.7 Concluding remarks.- 10. Experimental aeroelasticity.- 10.1 Review of structural dynamics experiments.- 10.2 Wind tunnel experiments.- 10.3 Flight experiments.- 10.4 The role of experimentation and theory in design.- 11. Nonlinear aeroelasticity.- Abstract.- 11.1 Introduction.- 11.2 The physical domain of nonlinear aeroelasticity.- 11.3 The mathematical consequences of nonlinearity.- 11.4 Representative results.- 11.5 The future.- 12. Aeroelastic control.- 12.1 Objectives and elements of aeroelastic control.- 12.2 Modeling for aeroelastic control.- 12.3 Control modeling of the typical section.- 12.4 Control design for the typical section.- Appendix I A primer for structural response to random pressure fluctuations.- References for Appendix I.- Appendix II Some example problems.
Recenzii
`... the text succeeds on three levels: as an introductory text for newcomers to aeroelasticity, as a reference text for professionals working in the field, and as a source book for researchers. The wide range of topics covered provides a fascinating insight into the cross-fertilization that can occur between seemingly disparate engineering disciplines ... There is little doubt that most workers in the field will wish to have access to this text.'
Journal of Sound and Vibration, 196:5 (1996)
Journal of Sound and Vibration, 196:5 (1996)