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MARC Lista (tabellare)
Advanced In-Flight Measurement Techniques / / edited by Fritz Boden, Nicholas Lawson, Henk W. Jentink, Jürgen Kompenhans
Advanced In-Flight Measurement Techniques / / edited by Fritz Boden, Nicholas Lawson, Henk W. Jentink, Jürgen Kompenhans
Edizione [1st ed. 2013.]
Pubbl/distr/stampa Berlin, Heidelberg : , : Springer Berlin Heidelberg : , : Imprint : Springer, , 2013
Descrizione fisica 1 online resource (xix, 344 pages) : illustrations (some color)
Disciplina 629.134
629.134/53
629.13453
Altri autori (Persone) BodenFritz
Collana Research Topics in Aerospace
Soggetto topico Aerospace engineering
Astronautics
Fluid mechanics
Physics
Thermodynamics
Heat engineering
Heat - Transmission
Mass transfer
Multibody systems
Vibration
Mechanics, Applied
Aerospace Technology and Astronautics
Engineering Fluid Dynamics
Applied and Technical Physics
Engineering Thermodynamics, Heat and Mass Transfer
Multibody Systems and Mechanical Vibrations
ISBN 9783642347382
364234738X
9781299336650
1299336655
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Part I – Introduction -- Part II – Wing Deformation Studies -- Part III – Propeller Deformation Studies -- Part IV – Helicopter Investigations -- Part V – Flow Measurements.
Record Nr. UNINA-9910437898203321
Berlin, Heidelberg : , : Springer Berlin Heidelberg : , : Imprint : Springer, , 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Introduction to flight testing / / James W. Gregory, Tianshu Liu
Introduction to flight testing / / James W. Gregory, Tianshu Liu
Autore Gregory James W.
Edizione [First edition.]
Pubbl/distr/stampa Hoboken, New Jersey : , : Wiley, , [2021]
Descrizione fisica 1 online resource (355 pages)
Disciplina 629.13453
Collana Aerospace Ser.
Soggetto topico Airplanes - Flight testing
ISBN 1-118-94980-3
1-118-94979-X
1-118-94981-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Cover -- Title Page -- Copyright -- Contents -- About the Authors -- Series Preface -- Preface -- Acknowledgements -- About the Companion Website -- Chapter 1 Introduction -- 1.1 Case Study: Supersonic Flight in the Bell XS‐1 -- 1.2 Types of Flight Testing -- 1.2.1 Scientific Research -- 1.2.2 Experimental Flight Test -- 1.2.3 Developmental Test and Evaluation -- 1.2.4 Operational Test and Evaluation -- 1.2.5 Airworthiness Certification -- 1.3 Objectives and Organization of this Book -- References -- Chapter 2 The Flight Environment: Standard Atmosphere -- 2.1 Earth's Atmosphere -- 2.2 Standard Atmosphere Model -- 2.2.1 Hydrostatics -- 2.2.2 Gravitational Acceleration and Altitude Definitions -- 2.2.3 Temperature -- 2.2.4 Viscosity -- 2.2.5 Pressure and Density -- 2.2.6 Operationalizing the Standard Atmosphere -- 2.2.7 Comparison with Experimental Data -- 2.3 Altitudes Used in Aviation -- References -- Chapter 3 Aircraft and Flight Test Instrumentation -- 3.1 Traditional Cockpit Instruments -- 3.1.1 Gyroscopic‐Based Instruments -- 3.1.2 Pressure‐Based Instruments -- 3.1.3 Outside Air Temperature -- 3.1.4 Other Instrumentation -- 3.2 Glass Cockpit Instruments -- 3.3 Flight Test Instrumentation -- 3.3.1 Global Navigation Satellite System -- 3.3.2 Accelerometers -- 3.3.3 Gyroscopes -- 3.3.4 Magnetometers -- 3.3.5 Barometer -- 3.3.6 Fusion of Sensor Data Streams -- 3.4 Summary -- References -- Chapter 4 Data Acquisition and Analysis -- 4.1 Temporal and Spectral Analysis -- 4.2 Filtering -- 4.3 Digital Sampling: Bit Depth Resolution and Sample Rate -- 4.4 Aliasing -- 4.5 Flight Testing Example -- 4.6 Summary -- References -- Chapter 5 Uncertainty Analysis -- 5.1 Error Theory -- 5.1.1 Types of Errors -- 5.1.2 Statistics of Random Error -- 5.1.3 Sensitivity Analysis and Uncertainty Propagation -- 5.1.4 Overall Uncertainty Estimate.
5.1.5 Chauvenet's Criterion for Outliers -- 5.1.6 Monte Carlo Simulation -- 5.2 Basic Error Sources in Flight Testing -- 5.2.1 Uncertainty of Flight Test Instrumentation -- 5.2.2 Example: Uncertainty in Density (Traditional Approach) -- 5.2.3 Example: Uncertainty in True Airspeed (Monte Carlo Approach) -- References -- Chapter 6 Flight Test Planning -- 6.1 Flight Test Process -- 6.2 Risk Management -- 6.3 Case Study: Accept No Unnecessary Risk -- 6.4 Individual Flight Planning -- 6.4.1 Flight Area and Airspace -- 6.4.2 Weather and NOTAMs -- 6.4.3 Weight and Balance -- 6.4.4 Airplane Pre‐Flight -- 6.5 Conclusion -- References -- Chapter 7 Drag Polar Measurement in Level Flight -- 7.1 Theory -- 7.1.1 Drag Polar and Power Required for Level Flight -- 7.1.2 The PIW-VIW Method -- 7.1.3 Internal Combustion Engine Performance Additional details are available in an online supplement, "Basic Performance Prediction of Internal Combustion Engines." -- 7.1.4 Propeller Performance -- 7.2 Flight Testing Procedures -- 7.3 Flight Test Example: Cirrus SR20 -- References -- Chapter 8 Airspeed Calibration -- 8.1 Theory -- 8.1.1 True Airspeed -- 8.1.2 Equivalent Airspeed -- 8.1.3 Calibrated Airspeed -- 8.1.4 Indicated Airspeed -- 8.1.5 Summary -- 8.2 Measurement Errors -- 8.2.1 Instrument Error -- 8.2.2 System Lag -- 8.2.3 Position Error -- 8.3 Airspeed Calibration Methods -- 8.3.1 Boom‐Mounted Probes -- 8.3.2 Trailing Devices and Pacer Aircraft -- 8.3.3 Ground‐Based Methods -- 8.3.4 Global Positioning System Method -- 8.4 Flight Testing Procedures -- 8.5 Flight Test Example: Cirrus SR20 -- References -- Chapter 9 Climb Performance and Level Acceleration to Measure Excess Power -- 9.1 Theory -- 9.1.1 Steady Climbs -- 9.1.2 Energy Methods -- 9.2 Flight Testing Procedures -- 9.2.1 Direct Measurement of Rate of Climb -- 9.2.2 Measurement of Level Acceleration.
9.3 Data Analysis -- 9.4 Flight Test Example: Cirrus SR20 -- References -- Chapter 10 Glide Speed and Distance -- 10.1 Theory -- 10.1.1 Drag Polar -- 10.1.2 Gliding Flight -- 10.1.3 Glide Hodograph -- 10.1.4 Best Glide Condition -- 10.2 Flight Testing Procedures -- 10.3 Data Analysis -- 10.4 Flight Test Example: Cirrus SR20 -- References -- Chapter 11 Takeoff and Landing -- 11.1 Theory -- 11.1.1 Takeoff Ground Roll -- 11.1.2 Landing Ground Roll -- 11.1.3 Rotation Distance -- 11.1.4 Transition Distance -- 11.1.5 Climb Distance -- 11.1.6 Total Takeoff and Landing Distances -- 11.1.7 Simple Estimations -- 11.2 Measurement Methods -- 11.3 Flight Testing Procedures -- 11.3.1 Standard Flight Procedures -- 11.3.2 Flight Test Procedures -- 11.3.3 Data Acquisition -- 11.3.4 Data Analysis -- 11.4 Flight Test Example: Cessna R182 -- References -- Chapter 12 Stall Speed -- 12.1 Theory -- 12.1.1 Viscous Boundary Layers -- 12.1.2 Flow Separation -- 12.1.3 Two‐Dimensional Stall Characteristics -- 12.1.4 Three‐Dimensional Stall Characteristics -- 12.1.5 Stall Control -- 12.1.6 Stall Prediction -- 12.2 Flight Testing Procedures -- 12.2.1 Flight Characteristics -- 12.2.2 Data Acquisition -- 12.3 Data Analysis -- 12.4 Flight Test Example: Cirrus SR20 -- References -- Chapter 13 Turning Flight -- 13.1 Theory -- 13.2 Flight Testing Procedures -- 13.2.1 Airworthiness Certification -- 13.2.2 Educational Flight Testing -- 13.2.3 Piloting -- 13.2.4 Instrumentation and Data Recording -- 13.3 Flight Test Example: Diamond DA40 -- References -- Chapter 14 Longitudinal Stability -- 14.1 Static Longitudinal Stability -- 14.1.1 Theory -- 14.1.2 Trim Condition -- 14.1.3 Flight Testing Procedures -- 14.1.4 Flight Test Example: Cirrus SR20 -- 14.2 Dynamic Longitudinal Stability -- 14.2.1 Theory -- 14.2.2 Flight Testing Procedures -- 14.2.3 Flight Test Example: Cirrus SR20.
References -- Chapter 15 Lateral‐Directional Stability -- 15.1 Static Lateral‐Directional Stability -- 15.1.1 Theory -- 15.1.2 Directional Stability -- 15.1.3 Lateral Stability -- 15.1.4 Flight Testing Procedures -- 15.1.5 Flight Testing Example: Cirrus SR20 -- 15.2 Dynamic Lateral‐Directional Stability -- 15.2.1 Theory -- 15.2.2 Flight Testing Procedures -- 15.2.3 Flight Test Example: Cirrus SR20 -- Nomenclature -- Acronyms and Abbreviations -- References -- Chapter 16 UAV Flight Testing1 -- 16.1 Overview of Unmanned Aircraft -- 16.2 UAV Design Principles and Features -- 16.2.1 Types of Airframes -- 16.2.2 UAV System Architecture -- 16.2.3 Electric Propulsion -- 16.2.4 Command and Control (C2) Link -- 16.2.5 Autonomy -- 16.3 Flight Regulations -- 16.4 Flight Testing Principles -- 16.4.1 Air Data Instrumentation -- 16.4.2 UAV Flight Test Planning -- 16.4.3 Piloting for UAV Flight Testing -- 16.5 Flight Testing Examples with the Peregrine UAS -- 16.5.1 Overview of the Peregrine UAS -- 16.5.2 Propulsion System Characterization -- 16.5.3 Specific Excess Power: Level Acceleration and Rate of Climb -- 16.5.4 Glide Flight Tests -- 16.6 Flight Testing Examples with the Avanti UAS -- 16.6.1 Overview of the Avanti UAS -- 16.6.2 Coast‐Down Testing for the Drag Polar -- 16.6.3 Radio Range Testing -- 16.6.4 Assessment of Autonomous System Performance -- 16.7 Conclusion -- References -- Appendix A Standard Atmosphere Tables -- Appendix B Useful Constants and Unit Conversion Factors -- Reference -- Appendix C Stability and Control Derivatives for a Notional GA Aircraft -- Reference -- Index -- EULA.
Record Nr. UNINA-9910555113303321
Gregory James W.  
Hoboken, New Jersey : , : Wiley, , [2021]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Introduction to flight testing / / James W. Gregory, Tianshu Liu
Introduction to flight testing / / James W. Gregory, Tianshu Liu
Autore Gregory James W.
Edizione [First edition.]
Pubbl/distr/stampa Hoboken, New Jersey : , : Wiley, , [2021]
Descrizione fisica 1 online resource (355 pages)
Disciplina 629.13453
Collana Aerospace
Soggetto topico Airplanes - Flight testing
ISBN 1-118-94980-3
1-118-94979-X
1-118-94981-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Cover -- Title Page -- Copyright -- Contents -- About the Authors -- Series Preface -- Preface -- Acknowledgements -- About the Companion Website -- Chapter 1 Introduction -- 1.1 Case Study: Supersonic Flight in the Bell XS‐1 -- 1.2 Types of Flight Testing -- 1.2.1 Scientific Research -- 1.2.2 Experimental Flight Test -- 1.2.3 Developmental Test and Evaluation -- 1.2.4 Operational Test and Evaluation -- 1.2.5 Airworthiness Certification -- 1.3 Objectives and Organization of this Book -- References -- Chapter 2 The Flight Environment: Standard Atmosphere -- 2.1 Earth's Atmosphere -- 2.2 Standard Atmosphere Model -- 2.2.1 Hydrostatics -- 2.2.2 Gravitational Acceleration and Altitude Definitions -- 2.2.3 Temperature -- 2.2.4 Viscosity -- 2.2.5 Pressure and Density -- 2.2.6 Operationalizing the Standard Atmosphere -- 2.2.7 Comparison with Experimental Data -- 2.3 Altitudes Used in Aviation -- References -- Chapter 3 Aircraft and Flight Test Instrumentation -- 3.1 Traditional Cockpit Instruments -- 3.1.1 Gyroscopic‐Based Instruments -- 3.1.2 Pressure‐Based Instruments -- 3.1.3 Outside Air Temperature -- 3.1.4 Other Instrumentation -- 3.2 Glass Cockpit Instruments -- 3.3 Flight Test Instrumentation -- 3.3.1 Global Navigation Satellite System -- 3.3.2 Accelerometers -- 3.3.3 Gyroscopes -- 3.3.4 Magnetometers -- 3.3.5 Barometer -- 3.3.6 Fusion of Sensor Data Streams -- 3.4 Summary -- References -- Chapter 4 Data Acquisition and Analysis -- 4.1 Temporal and Spectral Analysis -- 4.2 Filtering -- 4.3 Digital Sampling: Bit Depth Resolution and Sample Rate -- 4.4 Aliasing -- 4.5 Flight Testing Example -- 4.6 Summary -- References -- Chapter 5 Uncertainty Analysis -- 5.1 Error Theory -- 5.1.1 Types of Errors -- 5.1.2 Statistics of Random Error -- 5.1.3 Sensitivity Analysis and Uncertainty Propagation -- 5.1.4 Overall Uncertainty Estimate.
5.1.5 Chauvenet's Criterion for Outliers -- 5.1.6 Monte Carlo Simulation -- 5.2 Basic Error Sources in Flight Testing -- 5.2.1 Uncertainty of Flight Test Instrumentation -- 5.2.2 Example: Uncertainty in Density (Traditional Approach) -- 5.2.3 Example: Uncertainty in True Airspeed (Monte Carlo Approach) -- References -- Chapter 6 Flight Test Planning -- 6.1 Flight Test Process -- 6.2 Risk Management -- 6.3 Case Study: Accept No Unnecessary Risk -- 6.4 Individual Flight Planning -- 6.4.1 Flight Area and Airspace -- 6.4.2 Weather and NOTAMs -- 6.4.3 Weight and Balance -- 6.4.4 Airplane Pre‐Flight -- 6.5 Conclusion -- References -- Chapter 7 Drag Polar Measurement in Level Flight -- 7.1 Theory -- 7.1.1 Drag Polar and Power Required for Level Flight -- 7.1.2 The PIW-VIW Method -- 7.1.3 Internal Combustion Engine Performance Additional details are available in an online supplement, "Basic Performance Prediction of Internal Combustion Engines." -- 7.1.4 Propeller Performance -- 7.2 Flight Testing Procedures -- 7.3 Flight Test Example: Cirrus SR20 -- References -- Chapter 8 Airspeed Calibration -- 8.1 Theory -- 8.1.1 True Airspeed -- 8.1.2 Equivalent Airspeed -- 8.1.3 Calibrated Airspeed -- 8.1.4 Indicated Airspeed -- 8.1.5 Summary -- 8.2 Measurement Errors -- 8.2.1 Instrument Error -- 8.2.2 System Lag -- 8.2.3 Position Error -- 8.3 Airspeed Calibration Methods -- 8.3.1 Boom‐Mounted Probes -- 8.3.2 Trailing Devices and Pacer Aircraft -- 8.3.3 Ground‐Based Methods -- 8.3.4 Global Positioning System Method -- 8.4 Flight Testing Procedures -- 8.5 Flight Test Example: Cirrus SR20 -- References -- Chapter 9 Climb Performance and Level Acceleration to Measure Excess Power -- 9.1 Theory -- 9.1.1 Steady Climbs -- 9.1.2 Energy Methods -- 9.2 Flight Testing Procedures -- 9.2.1 Direct Measurement of Rate of Climb -- 9.2.2 Measurement of Level Acceleration.
9.3 Data Analysis -- 9.4 Flight Test Example: Cirrus SR20 -- References -- Chapter 10 Glide Speed and Distance -- 10.1 Theory -- 10.1.1 Drag Polar -- 10.1.2 Gliding Flight -- 10.1.3 Glide Hodograph -- 10.1.4 Best Glide Condition -- 10.2 Flight Testing Procedures -- 10.3 Data Analysis -- 10.4 Flight Test Example: Cirrus SR20 -- References -- Chapter 11 Takeoff and Landing -- 11.1 Theory -- 11.1.1 Takeoff Ground Roll -- 11.1.2 Landing Ground Roll -- 11.1.3 Rotation Distance -- 11.1.4 Transition Distance -- 11.1.5 Climb Distance -- 11.1.6 Total Takeoff and Landing Distances -- 11.1.7 Simple Estimations -- 11.2 Measurement Methods -- 11.3 Flight Testing Procedures -- 11.3.1 Standard Flight Procedures -- 11.3.2 Flight Test Procedures -- 11.3.3 Data Acquisition -- 11.3.4 Data Analysis -- 11.4 Flight Test Example: Cessna R182 -- References -- Chapter 12 Stall Speed -- 12.1 Theory -- 12.1.1 Viscous Boundary Layers -- 12.1.2 Flow Separation -- 12.1.3 Two‐Dimensional Stall Characteristics -- 12.1.4 Three‐Dimensional Stall Characteristics -- 12.1.5 Stall Control -- 12.1.6 Stall Prediction -- 12.2 Flight Testing Procedures -- 12.2.1 Flight Characteristics -- 12.2.2 Data Acquisition -- 12.3 Data Analysis -- 12.4 Flight Test Example: Cirrus SR20 -- References -- Chapter 13 Turning Flight -- 13.1 Theory -- 13.2 Flight Testing Procedures -- 13.2.1 Airworthiness Certification -- 13.2.2 Educational Flight Testing -- 13.2.3 Piloting -- 13.2.4 Instrumentation and Data Recording -- 13.3 Flight Test Example: Diamond DA40 -- References -- Chapter 14 Longitudinal Stability -- 14.1 Static Longitudinal Stability -- 14.1.1 Theory -- 14.1.2 Trim Condition -- 14.1.3 Flight Testing Procedures -- 14.1.4 Flight Test Example: Cirrus SR20 -- 14.2 Dynamic Longitudinal Stability -- 14.2.1 Theory -- 14.2.2 Flight Testing Procedures -- 14.2.3 Flight Test Example: Cirrus SR20.
References -- Chapter 15 Lateral‐Directional Stability -- 15.1 Static Lateral‐Directional Stability -- 15.1.1 Theory -- 15.1.2 Directional Stability -- 15.1.3 Lateral Stability -- 15.1.4 Flight Testing Procedures -- 15.1.5 Flight Testing Example: Cirrus SR20 -- 15.2 Dynamic Lateral‐Directional Stability -- 15.2.1 Theory -- 15.2.2 Flight Testing Procedures -- 15.2.3 Flight Test Example: Cirrus SR20 -- Nomenclature -- Acronyms and Abbreviations -- References -- Chapter 16 UAV Flight Testing1 -- 16.1 Overview of Unmanned Aircraft -- 16.2 UAV Design Principles and Features -- 16.2.1 Types of Airframes -- 16.2.2 UAV System Architecture -- 16.2.3 Electric Propulsion -- 16.2.4 Command and Control (C2) Link -- 16.2.5 Autonomy -- 16.3 Flight Regulations -- 16.4 Flight Testing Principles -- 16.4.1 Air Data Instrumentation -- 16.4.2 UAV Flight Test Planning -- 16.4.3 Piloting for UAV Flight Testing -- 16.5 Flight Testing Examples with the Peregrine UAS -- 16.5.1 Overview of the Peregrine UAS -- 16.5.2 Propulsion System Characterization -- 16.5.3 Specific Excess Power: Level Acceleration and Rate of Climb -- 16.5.4 Glide Flight Tests -- 16.6 Flight Testing Examples with the Avanti UAS -- 16.6.1 Overview of the Avanti UAS -- 16.6.2 Coast‐Down Testing for the Drag Polar -- 16.6.3 Radio Range Testing -- 16.6.4 Assessment of Autonomous System Performance -- 16.7 Conclusion -- References -- Appendix A Standard Atmosphere Tables -- Appendix B Useful Constants and Unit Conversion Factors -- Reference -- Appendix C Stability and Control Derivatives for a Notional GA Aircraft -- Reference -- Index -- EULA.
Record Nr. UNINA-9910678174803321
Gregory James W.  
Hoboken, New Jersey : , : Wiley, , [2021]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Introduction to flight testing / / James W. Gregory, Tianshu Liu
Introduction to flight testing / / James W. Gregory, Tianshu Liu
Autore Gregory James W.
Edizione [First edition.]
Pubbl/distr/stampa Hoboken, New Jersey : , : Wiley, , [2021]
Descrizione fisica 1 online resource (355 pages)
Disciplina 629.13453
Collana Aerospace
Soggetto topico Airplanes - Flight testing
ISBN 1-118-94980-3
1-118-94979-X
1-118-94981-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto Cover -- Title Page -- Copyright -- Contents -- About the Authors -- Series Preface -- Preface -- Acknowledgements -- About the Companion Website -- Chapter 1 Introduction -- 1.1 Case Study: Supersonic Flight in the Bell XS‐1 -- 1.2 Types of Flight Testing -- 1.2.1 Scientific Research -- 1.2.2 Experimental Flight Test -- 1.2.3 Developmental Test and Evaluation -- 1.2.4 Operational Test and Evaluation -- 1.2.5 Airworthiness Certification -- 1.3 Objectives and Organization of this Book -- References -- Chapter 2 The Flight Environment: Standard Atmosphere -- 2.1 Earth's Atmosphere -- 2.2 Standard Atmosphere Model -- 2.2.1 Hydrostatics -- 2.2.2 Gravitational Acceleration and Altitude Definitions -- 2.2.3 Temperature -- 2.2.4 Viscosity -- 2.2.5 Pressure and Density -- 2.2.6 Operationalizing the Standard Atmosphere -- 2.2.7 Comparison with Experimental Data -- 2.3 Altitudes Used in Aviation -- References -- Chapter 3 Aircraft and Flight Test Instrumentation -- 3.1 Traditional Cockpit Instruments -- 3.1.1 Gyroscopic‐Based Instruments -- 3.1.2 Pressure‐Based Instruments -- 3.1.3 Outside Air Temperature -- 3.1.4 Other Instrumentation -- 3.2 Glass Cockpit Instruments -- 3.3 Flight Test Instrumentation -- 3.3.1 Global Navigation Satellite System -- 3.3.2 Accelerometers -- 3.3.3 Gyroscopes -- 3.3.4 Magnetometers -- 3.3.5 Barometer -- 3.3.6 Fusion of Sensor Data Streams -- 3.4 Summary -- References -- Chapter 4 Data Acquisition and Analysis -- 4.1 Temporal and Spectral Analysis -- 4.2 Filtering -- 4.3 Digital Sampling: Bit Depth Resolution and Sample Rate -- 4.4 Aliasing -- 4.5 Flight Testing Example -- 4.6 Summary -- References -- Chapter 5 Uncertainty Analysis -- 5.1 Error Theory -- 5.1.1 Types of Errors -- 5.1.2 Statistics of Random Error -- 5.1.3 Sensitivity Analysis and Uncertainty Propagation -- 5.1.4 Overall Uncertainty Estimate.
5.1.5 Chauvenet's Criterion for Outliers -- 5.1.6 Monte Carlo Simulation -- 5.2 Basic Error Sources in Flight Testing -- 5.2.1 Uncertainty of Flight Test Instrumentation -- 5.2.2 Example: Uncertainty in Density (Traditional Approach) -- 5.2.3 Example: Uncertainty in True Airspeed (Monte Carlo Approach) -- References -- Chapter 6 Flight Test Planning -- 6.1 Flight Test Process -- 6.2 Risk Management -- 6.3 Case Study: Accept No Unnecessary Risk -- 6.4 Individual Flight Planning -- 6.4.1 Flight Area and Airspace -- 6.4.2 Weather and NOTAMs -- 6.4.3 Weight and Balance -- 6.4.4 Airplane Pre‐Flight -- 6.5 Conclusion -- References -- Chapter 7 Drag Polar Measurement in Level Flight -- 7.1 Theory -- 7.1.1 Drag Polar and Power Required for Level Flight -- 7.1.2 The PIW-VIW Method -- 7.1.3 Internal Combustion Engine Performance Additional details are available in an online supplement, "Basic Performance Prediction of Internal Combustion Engines." -- 7.1.4 Propeller Performance -- 7.2 Flight Testing Procedures -- 7.3 Flight Test Example: Cirrus SR20 -- References -- Chapter 8 Airspeed Calibration -- 8.1 Theory -- 8.1.1 True Airspeed -- 8.1.2 Equivalent Airspeed -- 8.1.3 Calibrated Airspeed -- 8.1.4 Indicated Airspeed -- 8.1.5 Summary -- 8.2 Measurement Errors -- 8.2.1 Instrument Error -- 8.2.2 System Lag -- 8.2.3 Position Error -- 8.3 Airspeed Calibration Methods -- 8.3.1 Boom‐Mounted Probes -- 8.3.2 Trailing Devices and Pacer Aircraft -- 8.3.3 Ground‐Based Methods -- 8.3.4 Global Positioning System Method -- 8.4 Flight Testing Procedures -- 8.5 Flight Test Example: Cirrus SR20 -- References -- Chapter 9 Climb Performance and Level Acceleration to Measure Excess Power -- 9.1 Theory -- 9.1.1 Steady Climbs -- 9.1.2 Energy Methods -- 9.2 Flight Testing Procedures -- 9.2.1 Direct Measurement of Rate of Climb -- 9.2.2 Measurement of Level Acceleration.
9.3 Data Analysis -- 9.4 Flight Test Example: Cirrus SR20 -- References -- Chapter 10 Glide Speed and Distance -- 10.1 Theory -- 10.1.1 Drag Polar -- 10.1.2 Gliding Flight -- 10.1.3 Glide Hodograph -- 10.1.4 Best Glide Condition -- 10.2 Flight Testing Procedures -- 10.3 Data Analysis -- 10.4 Flight Test Example: Cirrus SR20 -- References -- Chapter 11 Takeoff and Landing -- 11.1 Theory -- 11.1.1 Takeoff Ground Roll -- 11.1.2 Landing Ground Roll -- 11.1.3 Rotation Distance -- 11.1.4 Transition Distance -- 11.1.5 Climb Distance -- 11.1.6 Total Takeoff and Landing Distances -- 11.1.7 Simple Estimations -- 11.2 Measurement Methods -- 11.3 Flight Testing Procedures -- 11.3.1 Standard Flight Procedures -- 11.3.2 Flight Test Procedures -- 11.3.3 Data Acquisition -- 11.3.4 Data Analysis -- 11.4 Flight Test Example: Cessna R182 -- References -- Chapter 12 Stall Speed -- 12.1 Theory -- 12.1.1 Viscous Boundary Layers -- 12.1.2 Flow Separation -- 12.1.3 Two‐Dimensional Stall Characteristics -- 12.1.4 Three‐Dimensional Stall Characteristics -- 12.1.5 Stall Control -- 12.1.6 Stall Prediction -- 12.2 Flight Testing Procedures -- 12.2.1 Flight Characteristics -- 12.2.2 Data Acquisition -- 12.3 Data Analysis -- 12.4 Flight Test Example: Cirrus SR20 -- References -- Chapter 13 Turning Flight -- 13.1 Theory -- 13.2 Flight Testing Procedures -- 13.2.1 Airworthiness Certification -- 13.2.2 Educational Flight Testing -- 13.2.3 Piloting -- 13.2.4 Instrumentation and Data Recording -- 13.3 Flight Test Example: Diamond DA40 -- References -- Chapter 14 Longitudinal Stability -- 14.1 Static Longitudinal Stability -- 14.1.1 Theory -- 14.1.2 Trim Condition -- 14.1.3 Flight Testing Procedures -- 14.1.4 Flight Test Example: Cirrus SR20 -- 14.2 Dynamic Longitudinal Stability -- 14.2.1 Theory -- 14.2.2 Flight Testing Procedures -- 14.2.3 Flight Test Example: Cirrus SR20.
References -- Chapter 15 Lateral‐Directional Stability -- 15.1 Static Lateral‐Directional Stability -- 15.1.1 Theory -- 15.1.2 Directional Stability -- 15.1.3 Lateral Stability -- 15.1.4 Flight Testing Procedures -- 15.1.5 Flight Testing Example: Cirrus SR20 -- 15.2 Dynamic Lateral‐Directional Stability -- 15.2.1 Theory -- 15.2.2 Flight Testing Procedures -- 15.2.3 Flight Test Example: Cirrus SR20 -- Nomenclature -- Acronyms and Abbreviations -- References -- Chapter 16 UAV Flight Testing1 -- 16.1 Overview of Unmanned Aircraft -- 16.2 UAV Design Principles and Features -- 16.2.1 Types of Airframes -- 16.2.2 UAV System Architecture -- 16.2.3 Electric Propulsion -- 16.2.4 Command and Control (C2) Link -- 16.2.5 Autonomy -- 16.3 Flight Regulations -- 16.4 Flight Testing Principles -- 16.4.1 Air Data Instrumentation -- 16.4.2 UAV Flight Test Planning -- 16.4.3 Piloting for UAV Flight Testing -- 16.5 Flight Testing Examples with the Peregrine UAS -- 16.5.1 Overview of the Peregrine UAS -- 16.5.2 Propulsion System Characterization -- 16.5.3 Specific Excess Power: Level Acceleration and Rate of Climb -- 16.5.4 Glide Flight Tests -- 16.6 Flight Testing Examples with the Avanti UAS -- 16.6.1 Overview of the Avanti UAS -- 16.6.2 Coast‐Down Testing for the Drag Polar -- 16.6.3 Radio Range Testing -- 16.6.4 Assessment of Autonomous System Performance -- 16.7 Conclusion -- References -- Appendix A Standard Atmosphere Tables -- Appendix B Useful Constants and Unit Conversion Factors -- Reference -- Appendix C Stability and Control Derivatives for a Notional GA Aircraft -- Reference -- Index -- EULA.
Record Nr. UNINA-9910816370303321
Gregory James W.  
Hoboken, New Jersey : , : Wiley, , [2021]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Magnetic recording of flight test data / by G. E. Bennett
Magnetic recording of flight test data / by G. E. Bennett
Autore Bennett, G. E. <George Eric>
Pubbl/distr/stampa Neuilly sur Seine : Advisory group for aerospace research and development, 1974
Descrizione fisica V, 74 p. : ill. ; 30 cm
Disciplina 629.13453
Collana AGARD flight test instrumentation series
Soggetto non controllato Prove in volo dell'aeromobile
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-990008805110403321
Bennett, G. E. <George Eric>  
Neuilly sur Seine : Advisory group for aerospace research and development, 1974
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Symposium on Fatigue of Aircraft Structures
Symposium on Fatigue of Aircraft Structures
Pubbl/distr/stampa [Place of publication not identified], : American Society for Testing & Materials, 1960
Descrizione fisica 1 online resource (138 pages) : illustrations
Disciplina 629.13453
Collana ASTM special technical publication
Soggetto topico Airplanes - Testing
Strains and stresses
ISBN 0-8031-6746-6
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910164757503321
[Place of publication not identified], : American Society for Testing & Materials, 1960
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Un exemple de la determination des principaux coefficients aerodynamiques a partir des essais en vol : communication présentée à la session du Groupe de travail Essais en vol de l'AGARD tenue à Paris en avril 1958 / par G. Leblanc
Un exemple de la determination des principaux coefficients aerodynamiques a partir des essais en vol : communication présentée à la session du Groupe de travail Essais en vol de l'AGARD tenue à Paris en avril 1958 / par G. Leblanc
Autore Leblanc, Gildas
Pubbl/distr/stampa Paris : Groupe consultatif pour la recherche et la realisation aeronautiques, 1958
Descrizione fisica VI, 23 p. : ill. ; 28 cm
Disciplina 629.13453
Collana AGARD report
Soggetto non controllato Prove in volo - Aeromobile
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione fre
Altri titoli varianti An example of the determination of the principal aerodynamic coefficients from flight test results
Record Nr. UNINA-990008455990403321
Leblanc, Gildas  
Paris : Groupe consultatif pour la recherche et la realisation aeronautiques, 1958
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui