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Introduction to Flight Testing 요약정보 및 구매

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지은이 James W. Gregory,Tianshu Liu
발행년도 2021-05-01
판수 1판
페이지 352
ISBN 9781118949825
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  • Introduction to Flight Testing
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  • DESCRIPTION

    Introduction to Flight Testing

    Introduction to Flight Testing

    Provides an introduction to the basic flight testing methods employed on general aviation aircraft and unmanned aerial vehicles

    Introduction to Flight Testing provides a concise introduction to the basic flight testing methods employed on general aviation aircraft and unmanned aerial vehicles for courses in aeronautical engineering. There is particular emphasis on the use of modern on-board instruments and inexpensive, off-the-shelf portable devices that make flight testing accessible to nearly any student.

    This text presents a clear articulation of standard methods for measuring aircraft performance characteristics. Topics covered include aircraft and instruments, digital data acquisition techniques, flight test planning, the standard atmosphere, uncertainty analysis, level flight performance, airspeed calibration, stall, climb and glide, take-off and landing, level turn, static and dynamic longitudinal stability, lateral-directional stability, and flight testing of unmanned aircraft systems.

    Unique to this book is a detailed discussion of digital data acquisition (DAQ) techniques, which are an integral part of modern flight test programs. This treatment includes discussion of the analog-to-digital conversion, sample rate, aliasing, and filtering. These critical details provide the flight test engineer with the insight needed to understand the capabilities and limitations of digital DAQ.

    Key features:

    • Provides an introduction to the basic flight testing methods and instrumentation employed on general aviation aircraft and unmanned aerial vehicles.
    • Includes examples of flight testing on general aviation aircraft such as Cirrus, Diamond, and Cessna aircraft, along with unmanned aircraft vehicles.
    • Suitable for courses on Aircraft Flight Test Engineering.

    Introduction to Flight Testing provides resources and guidance for practitioners in the rapidly-developing field of drone performance flight test and the general aviation flight test community.

  • About the Authors xiii

    Series Preface xv

    Preface xvii

    Acknowledgements xxi

    About the Companion Website xxiii

    1 Introduction 1

    1.1 Case Study: Supersonic Flight in the Bell XS-1 3

    1.2 Types of Flight Testing 9

    1.2.1 Scientific Research 9

    1.2.2 Experimental Flight Test 12

    1.2.3 Developmental Test and Evaluation 14

    1.2.4 Operational Test and Evaluation 14

    1.2.5 Airworthiness Certification 15

    1.3 Objectives and Organization of this Book 17

    Nomenclature 18

    Acronyms and Abbreviations 19

    References 19

    2 The Flight Environment: Standard Atmosphere 22

    2.1 Earth’s Atmosphere 23

    2.2 Standard Atmosphere Model 24

    2.2.1 Hydrostatics 24

    2.2.2 Gravitational Acceleration and Altitude Definitions 25

    2.2.3 Temperature 26

    2.2.4 Viscosity 27

    2.2.5 Pressure and Density 28

    2.2.6 Operationalizing the Standard Atmosphere 29

    2.2.7 Comparison with Experimental Data 30

    2.3 Altitudes Used in Aviation 32

    Nomenclature 34

    Subscripts 34

    Acronyms and Abbreviations 35

    References 35

    3 Aircraft and Flight Test Instrumentation 36

    3.1 Traditional Cockpit Instruments 36

    3.1.1 Gyroscopic-Based Instruments 38

    3.1.2 Pressure-Based Instruments 38

    3.1.3 Outside Air Temperature 41

    3.1.4 Other Instrumentation 42

    3.2 Glass Cockpit Instruments 42

    3.3 Flight Test Instrumentation 45

    3.3.1 Global Navigation Satellite System 46

    3.3.2 Accelerometers 49

    3.3.3 Gyroscopes 49

    3.3.4 Magnetometers 50

    3.3.5 Barometer 51

    3.3.6 Fusion of Sensor Data Streams 51

    3.4 Summary 52

    Nomenclature 54

    Subscripts 54

    Acronyms and Abbreviations 54

    References 55

    4 Data Acquisition and Analysis 56

    4.1 Temporal and Spectral Analysis 56

    4.2 Filtering 61

    4.3 Digital Sampling: Bit Depth Resolution and Sample Rate 63

    4.4 Aliasing 66

    4.5 Flight Testing Example 69

    4.6 Summary 69

    Nomenclature 70

    Subscripts 70

    Acronyms and Abbreviations 70

    References 71

    5 Uncertainty Analysis 72

    5.1 Error Theory 73

    5.1.1 Types of Errors 73

    5.1.2 Statistics of Random Error 76

    5.1.3 Sensitivity Analysis and Uncertainty Propagation 77

    5.1.4 Overall Uncertainty Estimate 79

    5.1.5 Chauvenet’s Criterion for Outliers 79

    5.1.6 Monte Carlo Simulation 80

    5.2 Basic Error Sources in Flight Testing 81

    5.2.1 Uncertainty of Flight Test Instrumentation 81

    5.2.2 Example: Uncertainty in Density (Traditional Approach) 85

    5.2.3 Example: Uncertainty in True Airspeed (Monte Carlo Approach) 86

    Nomenclature 88

    Subscripts 89

    Acronyms and Abbreviations 89

    References 89

    6 Flight Test Planning 90

    6.1 Flight Test Process 90

    6.2 Risk Management 93

    6.3 Case Study: Accept No Unnecessary Risk 96

    6.4 Individual Flight Planning 97

    6.4.1 Flight Area and Airspace 98

    6.4.2 Weather and NOTAMs 99

    6.4.3 Weight and Balance 100

    6.4.4 Airplane Pre-Flight 103

    6.5 Conclusion 105

    Nomenclature 105

    Acronyms and Abbreviations 105

    References 105

    7 Drag Polar Measurement in Level Flight 107

    7.1 Theory 107

    7.1.1 Drag Polar and Power Required for Level Flight 107

    7.1.2 The PIW–VIW Method 112

    7.1.3 Internal Combustion Engine Performance 114

    7.1.4 Propeller Performance 119

    7.2 Flight Testing Procedures 124

    7.3 Flight Test Example: Cirrus SR20 125

    Nomenclature 127

    Acronyms and Abbreviations 129

    References 129

    8 Airspeed Calibration 132

    8.1 Theory 132

    8.1.1 True Airspeed 134

    8.1.2 Equivalent Airspeed 134

    8.1.3 Calibrated Airspeed 135

    8.1.4 Indicated Airspeed 137

    8.1.5 Summary 137

    8.2 Measurement Errors 138

    8.2.1 Instrument Error 138

    8.2.2 System Lag 138

    8.2.3 Position Error 139

    8.3 Airspeed Calibration Methods 142

    8.3.1 Boom-Mounted Probes 143

    8.3.2 Trailing Devices and Pacer Aircraft 143

    8.3.3 Ground-Based Methods 145

    8.3.4 Global Positioning System Method 145

    8.4 Flight Testing Procedures 147

    8.5 Flight Test Example: Cirrus SR20 148

    Nomenclature 150

    Subscripts 151

    Acronyms and Abbreviations 151

    References 151

    9 Climb Performance and Level Acceleration to Measure Excess Power 153

    9.1 Theory 153

    9.1.1 Steady Climbs 154

    9.1.2 Energy Methods 160

    9.2 Flight Testing Procedures 165

    9.2.1 Direct Measurement of Rate of Climb 165

    9.2.2 Measurement of Level Acceleration 166

    9.3 Data Analysis 167

    9.4 Flight Test Example: Cirrus SR20 168

    Nomenclature 172

    Subscripts 173

    Acronyms and Abbreviations 173

    References 174

    10 Glide Speed and Distance 175

    10.1 Theory 176

    10.1.1 Drag Polar 176

    10.1.2 Gliding Flight 179

    10.1.3 Glide Hodograph 180

    10.1.4 Best Glide Condition 181

    10.2 Flight Testing Procedures 183

    10.3 Data Analysis 185

    10.4 Flight Test Example: Cirrus SR20 186

    Nomenclature 188

    Subscripts 188

    Acronyms and Abbreviations 189

    References 189

    11 Takeoff and Landing 190

    11.1 Theory 190

    11.1.1 Takeoff Ground Roll 191

    11.1.2 Landing Ground Roll 193

    11.1.3 Rotation Distance 194

    11.1.4 Transition Distance 194

    11.1.5 Climb Distance 195

    11.1.6 Total Takeoff and Landing Distances 195

    11.1.7 Simple Estimations 195

    11.2 Measurement Methods 196

    11.3 Flight Testing Procedures 197

    11.3.1 Standard Flight Procedures 197

    11.3.2 Flight Test Procedures 199

    11.3.3 Data Acquisition 200

    11.3.4 Data Analysis 200

    11.4 Flight Test Example: Cessna R182 201

    Nomenclature 202

    Subscripts 203

    Acronyms and Abbreviations 204

    References 204

    12 Stall Speed 205

    12.1 Theory 206

    12.1.1 Viscous Boundary Layers 207

    12.1.2 Flow Separation 208

    12.1.3 Two-Dimensional Stall Characteristics 209

    12.1.4 Three-Dimensional Stall Characteristics 211

    12.1.5 Stall Control 211

    12.1.6 Stall Prediction 213

    12.2 Flight Testing Procedures 214

    12.2.1 Flight Characteristics 214

    12.2.2 Data Acquisition 216

    12.3 Data Analysis 217

    12.4 Flight Test Example: Cirrus SR20 219

    Nomenclature 221

    Subscripts 222

    Acronyms and Abbreviations 222

    References 222

    13 Turning Flight 224

    13.1 Theory 224

    13.2 Flight Testing Procedures 232

    13.2.1 Airworthiness Certification 232

    13.2.2 Educational Flight Testing 233

    13.2.3 Piloting 233

    13.2.4 Instrumentation and Data Recording 234

    13.3 Flight Test Example: Diamond DA40 235

    Nomenclature 236

    Subscripts 237

    Acronyms and Abbreviations 237

    References 237

    14 Longitudinal Stability 238

    14.1 Static Longitudinal Stability 238

    14.1.1 Theory 238

    14.1.2 Trim Condition 242

    14.1.3 Flight Testing Procedures 244

    14.1.4 Flight Test Example: Cirrus SR20 245

    14.2 Dynamic Longitudinal Stability 246

    14.2.1 Theory 246

    14.2.2 Flight Testing Procedures 254

    14.2.3 Flight Test Example: Cirrus SR20 255

    Nomenclature 257

    Subscripts 259

    Acronyms and Abbreviations 259

    References 259

    15 Lateral-Directional Stability 261

    15.1 Static Lateral-Directional Stability 261

    15.1.1 Theory 261

    15.1.2 Directional Stability 264

    15.1.3 Lateral Stability 265

    15.1.4 Flight Testing Procedures 266

    15.1.5 Flight Testing Example: Cirrus SR20 267

    15.2 Dynamic Lateral-Directional Stability 269

    15.2.1 Theory 269

    15.2.2 Flight Testing Procedures 272

    15.2.3 Flight Test Example: Cirrus SR20 272

    Nomenclature 274

    Acronyms and Abbreviations 275

    References 275

    16 UAV Flight Testing 277

    16.1 Overview of Unmanned Aircraft 277

    16.2 UAV Design Principles and Features 279

    16.2.1 Types of Airframes 280

    16.2.2 UAV System Architecture 281

    16.2.3 Electric Propulsion 285

    16.2.4 Command and Control (C2) Link 286

    16.2.5 Autonomy 287

    16.3 Flight Regulations 288

    16.4 Flight Testing Principles 288

    16.4.1 Air Data Instrumentation 289

    16.4.2 UAV Flight Test Planning 290

    16.4.3 Piloting for UAV Flight Testing 290

    16.5 Flight Testing Examples with the Peregrine UAS 291

    16.5.1 Overview of the Peregrine UAS 291

    16.5.2 Propulsion System Characterization 293

    16.5.3 Specific Excess Power: Level Acceleration and Rate of Climb 294

    16.5.4 Glide Flight Tests 296

    16.6 Flight Testing Examples with the Avanti UAS 299

    16.6.1 Overview of the Avanti UAS 299

    16.6.2 Coast-Down Testing for the Drag Polar 301

    16.6.3 Radio Range Testing 303

    16.6.4 Assessment of Autonomous System Performance 305

    16.7 Conclusion 305

    Nomenclature 307

    Acronyms and Abbreviations 307

    References 308

    Appendix A Standard Atmosphere Tables 310

    Appendix B Useful Constants and Unit Conversion Factors 313

    Reference 317

    Appendix C Stability and Control Derivatives for a Notional GA Aircraft 318

    Reference 319

    Index 321

  • James W. Gregory is an associate professor in the Department of Mechanical and Aerospace Engineering, and Associate Director for UAS of the Aerospace Research Center at The Ohio State University. He received his Bachelor of Aerospace Engineering from Georgia Tech, and masters and doctorate degrees in Aeronautics and Astronautics from Purdue University. His research interests focus on development of pressure-sensitive paint as an advanced measurement technique, drag reduction of bluff body wakes via aerodynamic flow control, and flight testing of unmanned aircraft systems. His work experience includes stints at the US Air Force Research Laboratory Air Vehicles Directorate, the US Air Force Academy, Delta Air Lines, NASA Glenn Research Center, Tohoku University in Japan, and as a Fulbright Scholar at the Technion in Israel. He is an instrument-rated private pilot.

    Tianshu Liu is a professor and the director of Applied Aerodynamics Laboratory at Western Michigan University.  He received a Ph.D. in aeronautics and astronautics from Purdue University in 1996.  He was a research scientist at NASA Langley Research Center in 1999-2004.  His research areas are experimental and applied aerodynamics and fluid mechanics.  In particular, he has contributed to image-based measurement techniques for various physical quantities such as surface pressure, temperature/heat-transfer, skin friction, velocity fields, aeroelastic deformation, and distributed and integrated forces.  His topics also include videogrammetry and vision for aerospace applications, flow control, flapping flight, flight vehicle design, turbulence and transition, and flight tests. 

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  • Introduction to Flight Testing
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