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1. |
Record Nr. |
UNINA9910139752303321 |
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Autore |
Hopkins Bruce R |
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Titolo |
Fundraising law made easy [[electronic resource] /] / Bruce R. Hopkins |
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Pubbl/distr/stampa |
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Hoboken, N.J., : John Wiley & Sons, c2009 |
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ISBN |
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0-470-53024-3 |
1-282-27946-7 |
9786612279461 |
1-118-38634-5 |
0-470-53022-7 |
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Descrizione fisica |
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1 online resource (381 p.) |
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Disciplina |
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Soggetti |
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Fund raising - Law and legislation - United States |
Charitable uses, trusts, and foundations - United States |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Nota di contenuto |
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Fundraising Law Made Easy; Contents; Preface; About the Author; Chapter 1: INTRODUCTION TO THE LAW OF FUNDRAISING FOR CHARITY; Chapter 2: FUNDRAISERS' LAW PRIMER; Chapter 3: STATE REGULATION OF CHARITABLE FUNDRAISING; Chapter 4: PUBLIC CHARITIES AND PRIVATE FOUNDATIONS; Chapter 5: FEDERAL ANNUAL REPORTING REQUIREMENTS; Chapter 6: CHARITABLE GIVING RULES; Chapter 7: UNRELATED BUSINESS RULES; Chapter 8: OTHER FEDERAL TAX LAW REGULATION OF FUNDRAISING; Chapter 9: FUNDRAISING AND CONSTITUTIONAL LAW; Chapter 10: FUNDRAISING AND GOVERNANCE; Chapter 11: FUNDRAISING AND IRS AUDITS |
Chapter 12: PERSPECTIVES AND COMMENTARIESIndex |
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Sommario/riassunto |
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The ins and outs of fundraising law-made easy-from nonprofit law authority Bruce Hopkins Author Bruce R. Hopkins-a leading authority on the laws regulating fundraising-offers essential, practical legal information in easy-to-understand English. His practical tips and ""red flags"" provide useful advice and present critical information in an efficient and comprehensible fashion. Now your organization can be fully informed about the basic legal requirements affecting fundraising and avoid the perils lurking in the myriad tax-law traps. Fundraising |
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Law Made Easy clearly shows yo |
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2. |
Record Nr. |
UNINA9910829075303321 |
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Autore |
Hodges Dewey H. |
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Titolo |
Introduction to structural dynamics and aeroelasticity / / Dewey H. Hodges, G. Alvin Pierce |
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Pubbl/distr/stampa |
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Cambridge : , : Cambridge University Press, , 2011 |
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ISBN |
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1-139-92979-8 |
1-107-21462-9 |
1-139-11939-7 |
1-283-29847-3 |
9786613298478 |
1-139-12296-7 |
0-511-99711-6 |
1-139-11722-X |
1-139-12788-8 |
1-139-11069-1 |
1-139-11286-4 |
1-139-11505-7 |
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Edizione |
[Second edition.] |
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Descrizione fisica |
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1 online resource (xxi, 247 pages) : digital, PDF file(s) |
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Collana |
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Cambridge aerospace series ; ; 15 |
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Classificazione |
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Disciplina |
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Soggetti |
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Aeroelasticitat |
Vehicles espacials - Dinàmica |
Space vehicles - Dynamics |
Aeroelasticity |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Title from publisher's bibliographic system (viewed on 05 Oct 2015). |
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Nota di bibliografia |
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Includes bibliographical references and index. |
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Nota di contenuto |
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Cover; Title; Copyright; Contents; Figures; Tables; Foreword; From First Edition; Addendum for Second Edition; 1 Introduction; 2 Mechanics Fundamentals; 2.1 Particles and Rigid Bodies; 2.1.1 Newton's Laws; 2.1.2 Euler's Laws and Rigid Bodies; 2.1.3 Kinetic Energy; 2.1.4 Work; 2.1.5 Lagrange's Equations; 2.2 Modeling the Dynamics of Strings; |
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2.2.1 Equations of Motion; 2.2.2 Strain Energy; 2.2.3 Kinetic Energy; 2.2.4 Virtual Work of Applied, Distributed Force; 2.3 Elementary Beam Theory; 2.3.1 Torsion; 2.3.2 Bending; 2.4 Composite Beams |
2.4.1 Constitutive Law and Strain Energy for Coupled Bending and Torsion2.4.2 Inertia Forces and Kinetic Energy for Coupled Bending and Torsion; 2.4.3 Equations of Motion for Coupled Bending and Torsion; 2.5 The Notion of Stability; 2.6 Systems with One Degree of Freedom; 2.6.1 Unforced Motion; 2.6.2 Harmonically Forced Motion; 2.7 Epilogue; Problems; 3 Structural Dynamics; 3.1 Uniform String Dynamics; 3.1.1 Standing Wave (Modal) Solution; 3.1.2 Orthogonality of Mode Shapes; 3.1.3 Using Orthogonality; 3.1.4 Traveling Wave Solution; 3.1.5 Generalized Equations of Motion |
3.1.6 Generalized Force3.1.7 Example Calculations of Forced Response; 3.2 Uniform Beam Torsional Dynamics; 3.2.1 Equations of Motion; 3.2.2 Boundary Conditions; 3.2.3 Example Solutions for Mode Shapes and Frequencies; 3.2.4 Calculation of Forced Response; 3.3 Uniform Beam Bending Dynamics; 3.3.1 Equation of Motion; 3.3.2 General Solutions; 3.3.3 Boundary Conditions; 3.3.4 Example Solutions for Mode Shapes and Frequencies; 3.3.5 Calculation of Forced Response; 3.4 Free Vibration of Beams in Coupled Bending and Torsion; 3.4.1 Equations of Motion; 3.4.2 Boundary Conditions |
3.5 Approximate Solution Techniques3.5.1 The Ritz Method; 3.5.2 Galerkin's Method; 3.5.3 The Finite Element Method; 3.6 Epilogue; Problems; 4 Static Aeroelasticity; 4.1 Wind-Tunnel Models; 4.1.1 Wall-Mounted Model; 4.1.2 Sting-Mounted Model; 4.1.3 Strut-Mounted Model; 4.1.4 Wall-Mounted Model for Application to Aileron Reversal; 4.2 Uniform Lifting Surface; 4.2.1 Steady-Flow Strip Theory; 4.2.2 Equilibrium Equation; 4.2.3 Torsional Divergence; 4.2.4 Airload Distribution; 4.2.5 Aileron Reversal; 4.2.6 Sweep Effects; 4.2.7 Composite Wings and Aeroelastic Tailoring; 4.3 Epilogue; Problems |
5 Aeroelastic Flutter5.1 Stability Characteristics from Eigenvalue Analysis; 5.2 Aeroelastic Analysis of a Typical Section; 5.3 Classical Flutter Analysis; 5.3.1 One-Degree-of-Freedom Flutter; 5.3.2 Two-Degree-of-Freedom Flutter; 5.4 Engineering Solutions for Flutter; 5.4.1 The k Method; 5.4.2 The p-k Method; 5.5 Unsteady Aerodynamics; 5.5.1 Theodorsen's Unsteady Thin-Airfoil Theory; 5.5.2 Finite-State Unsteady Thin-Airfoil Theory of Peters et al.; 5.6 Flutter Prediction via Assumed Modes; 5.7 Flutter Boundary Characteristics; 5.8 Structural Dynamics, Aeroelasticity, and Certification |
5.8.1 Ground-Vibration Tests |
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Sommario/riassunto |
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This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal representation and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter and elastic tailoring. More than one hundred illustrations and tables help clarify the text and more than fifty problems enhance student learning. This text meets the need for an up-to-date treatment of structural dynamics and aeroelasticity for advanced undergraduate or beginning graduate aerospace engineering students. |
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