Virtual Principles in Aircraft Structures: Mechanics of Structural Systems, cartea 6-7
Autor M. Gatewooden Limba Engleză Paperback – 23 aug 2014
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Specificații
ISBN-13: 9789401070188
ISBN-10: 9401070180
Pagini: 740
Ilustrații: XXXIII, 695 p. 69 illus. In 2 volumes, not available separately.
Dimensiuni: 155 x 235 x 39 mm
Ediția:Softcover reprint of the original 1st ed. 1989
Editura: SPRINGER NETHERLANDS
Colecția Springer
Seria Mechanics of Structural Systems
Locul publicării:Dordrecht, Netherlands
ISBN-10: 9401070180
Pagini: 740
Ilustrații: XXXIII, 695 p. 69 illus. In 2 volumes, not available separately.
Dimensiuni: 155 x 235 x 39 mm
Ediția:Softcover reprint of the original 1st ed. 1989
Editura: SPRINGER NETHERLANDS
Colecția Springer
Seria Mechanics of Structural Systems
Locul publicării:Dordrecht, Netherlands
Public țintă
ResearchCuprins
1 / The basic three, two, and one dimensional equations in structural analysis.- 2 / Virtual displacement and virtual force methods in structural analysis.- 3 / The virtual principles for pin-jointed trusses.- 4 / The virtual principles for simple beams.- 5 / Box beam shear stresses and deflections.- 6 / Shear lag in thin web structures.- 1 / Allowable stresses of flight vehicle materials.- 2 / Analysis and design of joints and splices.- 3 / Structural design of aircraft components.- 4 / Analysis and design of pressurized structures.- 5 / Approximate solutions using the virtual principles.- 6 / Dynamics of simple beams.- 7 / The plate equations.- 8 / Approximate matrix equations for plate finite elements.- 9 / Matrix structural analysis using finite elements.- 10 / Composite Materials.- Appendix A / Notes on matrix algebra.- A.1 Definition of matrices.- A.2 Addition, subtraction, multiplication of matrices.- A.3 Determinants.- A.4 Matrix inversion.- A.5 Solution of systems of simultaneous equations by matrices.- A.6 Solution of systems of simultaneous equations by tri-diagonal matrices.- A.7 Solution of systems of equations by Jordan successive transformations.- A.8 Matrix representations.- A.9 Orthogonal matrices.- A.10 Eigenvalues and eigenvectors of matrices.- A.11 Note on matrix notation.- References.- Appendix B / External forces on flight vehicles.- B.1 Introduction.- B.2 Inertial forces for rigid body translation and rotation in a vertical plane.- B.3 Air forces on airplane wing.- B.4 Airplane equilibrium equations in flight. Load factors.- B.6 Wing spanwise lift coefficient distribution.- B.7 Spanwise lift coefficient distribution on twisted wings.- B.8 Spanwise airload, shear, and moment distributions on wing.- B.9 Distribution of inertia forces on wing and fuselage.- B.10 Forces and moments on landing gear structures.- B.11 Thermal forces.- B.12 Miscellaneous forces.- B.13 Deflection effects on the external forces.- B.14 Criteria for the structure to support the external forces.- B.15 Problems.- References.- Appendix C / Derivation of the strain energy theorems from the virtual principles.- C.1 Work and strain energy.- C.2 Maximum and minimum strain energy and total potential energy.- C.3 Theorem of minimum total potential energy.- C.4 Theorem of minimum strain energy.- C.5 Castigliano’s theorem (Part I).- C.6 Hamilton’s principle.- C.7 Theorem of minimum total complementary potential theory.- C.8 Theorem of minimum complementary strain energy.- C.9 Castigliano’s theorem (Part II).- C.10 Reissner’s variational principle.- C.11 Comparison of the virtual principles and the strain energy theorems.- References.