Javidinejad | Standard Methods for Aerospace Stress Analysis | Buch | 978-1-394-33018-8 | www.sack.de

Buch, Englisch, 272 Seiten, Format (B × H): 183 mm x 257 mm, Gewicht: 726 g

Javidinejad

Standard Methods for Aerospace Stress Analysis


1. Auflage 2025
ISBN: 978-1-394-33018-8
Verlag: Wiley

Buch, Englisch, 272 Seiten, Format (B × H): 183 mm x 257 mm, Gewicht: 726 g

ISBN: 978-1-394-33018-8
Verlag: Wiley


Standard Methods for Aerospace Stress Analysis

Create safer, more reliable planes with this crucial guide

Aerospace Stress Analysis is the field of research and engineering that evaluates stresses and strains on aerospace structures. By analyzing how different materials and components respond to forces, it helps aerospace engineers build for structural integrity and safety. Combining mathematical and computational models with experimental techniques, it’s a crucial component of developing viable aerospace technologies.

Standard Methods for Aerospace Stress Analysis offers a thorough, practical overview of the structural and stress analysis of both principal and secondary aircraft structures. It covers both fundamental concepts and advanced computational methods, along with key applications. With coverage of both interior and exterior structures, it’s a one-stop shop for all major aspects of stress analysis.

Standard Methods for Aerospace Stress Analysis features: - Step-by-step examples for every aircraft section
- Detailed discussion of methods including Finite Element Analysis
- An overview of key information on static, fatigue, damage tolerance, buckling, and more

Standard Methods for Aerospace Stress Analysis is ideal for professional mechanical and aerospace engineers working in the aircraft or space industries, as well as students in the field.

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Autoren/Hrsg.


Weitere Infos & Material


List of Figures xiii

List of Tables xvii

About the Author xix

Preface xxi

About the Companion Website xxiii

1 Stress Analysis 1

1.1 Introduction to Stress Analysis 1

1.2 The Material Definitions 1

1.3 Stress–Strain Curves for Ductile Material 3

1.4 Stress–Strain Curve for Brittle Material 45

1.5 The General Methods 47

1.6 The Structure of Stress Reports 47

Problems 48

Bibliography 49

2 Aircraft and Fuselage Stress Idealization 51

2.1 Introduction to Aircraft and Fuselage Geometry 51

2.2 Idealization of Structure 56

2.3 Cross-Sectional Properties 56

2.3.1 Centroid 56

2.3.2 First Moment of Area 57

2.3.3 Second Moment of Inertia 57

2.3.4 Parallel Axis Theory 57

2.4 Stress Types 57

2.4.1 Tension 57

2.4.2 Compression 57

2.4.3 Shear 58

2.4.4 Combined Loading 58

2.4.5 Pressure 58

2.5 2D Stresses on an Inclined Angle 60

2.6 Principal Stresses 60

2.7 Mohr’s Circle 61

2.8 Plane Stress and Strain 64

2.9 Von Mises Stress 65

Problems 65

Bibliography 66

3 FEA Modeling Approach 67

3.1 Introduction to General FEA Modeling Approach 67

3.2 CAD Model to FEA Model Conversion 68

3.3 Loads Extractions 70

3.4 Stress on Truss Elements 70

3.5 Stress on Beam Members 81

3.6 Finite Element Analysis of Plates 83

3.7 Finite Element Analysis Results Correlations 84

3.8 Determination of Fastener Stiffness for FEA 85

3.9 FEA of Aircraft Wings 86

3.10 FEA of Interior Monuments 88

Problems 93

Bibliography 94

4 Energy Methods 97

4.1 Introduction to Energy Methods 97

4.2 Strain Energy 97

4.3 Castigliano’s Theory 98

Problems 102

Bibliography 103

5 Loads on Aircraft 105

5.1 Introduction to Loads Acting on Aircraft 105

5.2 Load Distribution and Boundary Conditions 106

5.3 Shear and Moment Diagrams 107

5.4 Bending of the Beams 113

5.5 Shear of the Beams 114

5.6 Shear Stresses due to Torsion 118

Problems 121

Bibliography 122

6 Aircraft Load Cases 123

6.1 Introduction to Load Cases 123

6.2 Aviation Loads Regulations 123

6.3 Limit and Ultimate Load Cases 123

6.4 Flight Loads 124

6.5 Maneuver Loads 124

6.6 Lateral gust 124

6.7 Design Fuel Loads 125

6.8 Ground Loads 125

6.9 Water Loads 125

6.10 Emergency Landing Load Cases 125

6.11 Side Loads 126

6.12 Pressurization 126

Bibliography 126

7 Stress Evaluation Methods 127

7.1 Introduction to Stress Evaluation Methodology 127

7.2 Structural Aspects of Design 127

7.2.1 Skin Membrane 127

7.3 Shear-Resistant Beams 133

7.4 Web Diagonal Tension 135

7.5 Web Shear Beam with Cutouts 138

7.6 Fatigue Analysis 141

7.7 Damage Tolerance 146

Problems 148

Bibliography 149

8 Composite Analysis 153

8.1 Introduction to Composite Analysis 153

8.2 Orthotropic Lamina 153

8.3 Orthotropic Layers Oriented at an Arbitrary Angle 154

8.4 Analysis of Laminate 157

8.5 Common Laminate Stack-Up Designations 160

8.6 Effective Modulus of the Laminate 164

8.7 Tsai Hill Failure Criteria 164

8.8 Tsai-Wu Failure Criteria 165

Problems 165

Bibliography 166

9 Corrosion 169

9.1 Introduction to Corrosion 169

9.2 Stress Corrosion 171

Bibliography 173

10 Joints and Fasteners 175

10.1 Introduction to Joints and Fasteners 175

10.2 Fastener-Connection Failure 175

10.2.1 Mechanical Joints (Lugs) Analysis 175

10.2.2 Mechanical Joints (Pin Bending) Analysis 177

10.3 Adhesive-Connection Failure 180

10.4 Eccentric Loading of Fasteners 181

10.5 Tension Clip Fastener Loads 183

10.6 Inter-Coupling Loading of Fasteners and Inserts 185

10.7 Welded-Connection Failure 188

10.8 Fastener Properties 188

Problems 192

Bibliography 193

11 Composite Testing Methods and Procedures 197

11.1 Introduction to Composite Testing Methods and Procedures 197

11.2 Uniaxial Tensile Test 197

11.3 (±45) Off-Axis Shear Test 198

11.4 Three-Point Bending 199

11.5 Four-Point Bending 201

11.6 Shear Testing of Sandwich Core Material 202

Bibliography 203

12 Elastic Stability and Buckling 205

12.1 Introduction to Elastic Stability 205

12.2 Column Buckling Instability 205

12.3 Column Buckling Under Combined Axial and Bending Loads 209

12.4 Multiple Column System Buckling 210

12.5 Buckling of Plates 212

12.6 Skin Inter-Rivet Buckling 215

12.7 Crippling of the Angle and Thin Complex Shapes 215

12.8 Buckling of Laminate Plates Under Axial Loading 217

12.9 Buckling of Sandwich Panels 220

12.10 Buckling of Thin Cylinder Shells 222

12.10.1 Buckling of Thin Cylinder Under External Radial Pressure 222

12.10.2 Buckling of Internally Pressurized Thin Cylinders Under Applied Axial Compressive Loading 223

12.10.3 Buckling of Unpressurized Thin Cylinders Under Applied Axial Compressive Loading 223

12.10.4 Buckling of Thin Cylinders Under Bending 224

12.10.5 Buckling of Internally Pressurized Thin Cylinders Under Bending Loading 224

Problems 226

Bibliography 227

13 Interior Monuments Analysis and Testing 231

13.1 Introduction to Interior Monuments 231

13.2 Analysis Methods 231

13.3 Testing Procedure and Requirements 233

13.4 Data Acquisition and Data Reduction 233

Bibliography 235

14 Dynamics and Vibration Aspects 237

14.1 Introduction to Dynamic and Vibration Aspects of the Structures 237

14.2 Fundamental Concepts 237

14.3 Analytical Methods for Plate Vibration 237

14.4 Computational Methods 238

Bibliography 240

Index 243


Amir Javidinejad received his Ph.D. in Mechanical Engineering from the University of Texas at Arlington, his M.S. in Engineering Mechanics from Georgia Institute of Technology, his B.S. in Mechanical Engineering from the University of Cincinnati, and holds a Certificate in Leadership Mastery from the UCLA-Extension. He has extensive experience in structural/solid mechanics, Finite Element Methods, machine design, and various other stress analysis methods from aerospace, military, and commercial industries, as well as from academia. His expertise and knowledge include space structures analysis, micro sensors analysis, rocket design analysis, helicopter structural repair analysis, airplane structures modifications, aircraft interior monument structures analysis, and certification and qualification testing. He has also been involved in research in the areas of structural mechanics of isotropic, anisotropic, and composite materials. Dr. Javidinejad is a Licensed Professional Mechanical Engineer in the State of California, License #38567, and in the State of Texas, License #141561. Dr. Javidinejad is a member of the Pi Tau Sigma mechanical engineering honor society, a member of the American Society of Mechanical Engineers (ASME), and a member of the American Society of Engineering Education (ASEE). Also, Dr. Javidinejad is currently a part-time Lecturer of Mechanical Engineering in the California State Polytechnic University, Pomona.



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