Flight dynamics:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Princeton, NJ [u.a.]
Princeton Univ. Pr.
2004
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XVIII, 845 S. graph. Darst. |
| ISBN: | 0691114072 |
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Datensatz im Suchindex
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| adam_text | FLIGHT DYNAMICS ROBERT F. STENGEL PRINCETON UNIVERSITY PRESS PRINCETON
AND OXFORD CONTENTS PREFACE XV CHAPTER ONE INTRODUCTION 1 1.1 ELEMENTS
OF THE AIRPLANE 1 AIRFRAME COMPONENTS 1 PROPULSION SYSTEMS 4 1.2
REPRESENTATIVE FLIGHT VEHICLES 6 LIGHT GENERAL AVIATION AIRCRAFT 6
VARIABLE-STABILITY RESEARCH AIRCRAFT 6 SAILPLANE 8 BUSINESS JET AIRCRAFT
9 TURBOPROP COMMUTER AIRCRAFT 10 SMALL COMMERCIAL TRANSPORT AIRCRAFT 10
LARGE COMMERCIAL TRANSPORT AIRCRAFT 12 SUPERSONIC TRANSPORT AIRCRAFT 14
FIGHTER/ATTACK AIRCRAFT 15 BOMBER AIRCRAFT 16 SPACE SHUTTLE 16
UNINHABITED AIR VEHICLE 18 1.3 THE MECHANICS OF FLIGHT 19 REFERENCES 27
CHAPTER TWO EXPLORING THE FLIGHT ENVELOPE 29 2.1 THE EARTH S ATMOSPHERE
30 PRESSURE, DENSITY, AND THE SPEED OF SOUND 32 VISCOSITY, HUMIDITY, AND
RAIN 33 WIND FIELDS AND ATMOSPHERIC TURBULENCE 34 VIII CONTENTS 2.2
KINEMATIC EQUATIONS 38 TRANSLATIONAL POSITION AND VELOCITY 39 ANGULAR
ORIENTATION AND RATE 42 AIRFLOW ANGLES 53 SUMMARY OF AXIS SYSTEMS AND
TRANSFORMATIONS 53 2.3 FORCES AND MOMENTS 59 ALTERNATIVE AXIS SYSTEMS 60
AERODYNAMIC FORCES AND MOMENTS 61 2.4 STATIC AERODYNAMIC COEFFICIENTS 65
LIFT 67 DRAG 76 PITCHING MOMENT 87 SIDE FORCE 96 YAWING MOMENT 97
ROLLING MOMENT 98 GROUND EFFECT 101 2.5 THRUSTING CHARACTERISTICS OF
AIRCRAFT POWERPLANTS 103 PROPELLERS 107 RECIPROCATING ENGINES 110
TURBOPROP, TURBOFAN, AND TURBOJET ENGINES 111 RAMJET AND SCRAMJET
ENGINES 115 GENERAL THRUST MODELS 117 2.6 STEADY FLIGHT PERFORMANCE 118
STRAIGHT AND LEVEL FLIGHT 119 STEADY FLIGHT ENVELOPE 124 CRUISING RANGE
128 GLIDING FLIGHT 130 CLIMBING FLIGHT 133 MANEUVERING ENVELOPE 135
STEADY TURNING FLIGHT 137 REFERENCES 141 CHAPTER THREE DYNAMICS OF
AIRCRAFT MOTION 147 3.1 MOMENTUM AND ENERGY 147 TRANSLATIONAL MOMENTUM,
WORK, ENERGY, AND POWER 148 ENERGY-CHANGING MANEUVERS 152 ANGULAR
MOMENTUM AND ENERGY 155 CONTENTS IX 3.2 DYNAMIC EQUATIONS FOR A FLAT
EARTH 159 RIGID-BODY DYNAMIC EQUATIONS 159 SCALAR EQUATIONS FOR A
SYMMETRIC AIRCRAFT 167 ALTERNATIVE FRAMES OF REFERENCE 169 INERTIAL
REFERENCE FRAMES 169 BODY-AXIS REFERENCE FRAMES 170 VELOCITY- AND
WIND-AXIS REFERENCE FRAMES 176 AIR-MASS-RELATIVE REFERENCE FRAME 180
DIRECTION COSINES AND QUATERNIONS 182 ACCELERATION SENSED AT AN
ARBITRARY POINT 187 3.3 DYNAMIC EQUATIONS FOR A ROUND, ROTATING EARTH
188 GEOMETRY AND GRAVITY FIELD OF THE EARTH 188 RIGID-BODY DYNAMIC
EQUATIONS 196 3.4 AERODYNAMIC EFFECTS OF ROTATIONAL AND UNSTEADY MOTION
199 PITCH-RATE EFFECTS 201 ANGLE-OF-ATTACK-RATE EFFECTS 204 YAW-RATE
EFFECTS 206 ROLL-RATE EFFECTS 208 EFFECTS OF WIND SHEAR AND WAKE
VORTICES 209 3.5 AERODYNAMIC EFFECTS OF CONTROL 214 ELEVATORS,
STABILATORS, ELEVONS, AND CANARDS 215 RUDDERS 216 AILERONS 217 SPOILERS
AND WING FLAPS 217 OTHER CONTROL DEVICES 218 ISOLATED CONTROL SURFACES
219 TRAILING-EDGE FLAPS 231 3.6 SOLUTION OF NONLINEAR DIFFERENTIAL
EQUATIONS 234 NUMERICAL ALGORITHMS FOR INTEGRATION 234 EQUATIONS OF
MOTION 240 REPRESENTATION OF DATA 242 TRIMMED SOLUTION OF THE EQUATIONS
OF MOTION 255 REFERENCES 266 CONTENTS CHAPTER FOUR METHODS OF ANALYSIS
AND DESIGN 273 4.1 LOCAL LINEARIZATION OF DIFFERENTIAL EQUATIONS 274
STABILITY AND CONTROL DERIVATIVES 277 INCORPORATING UNSTEADY AERODYNAMIC
EFFECTS 284 SYMMETRIC AIRCRAFT IN WINGS-LEVEL FLIGHT 285 LONGITUDINAL
EQUATIONS OF MOTION 289 LATERAL-DIRECTIONAL EQUATIONS OF MOTION 290
STABILITY-AXIS EQUATIONS OF MOTION 291 4.2 SOLUTION OF LINEAR
DIFFERENTIAL EQUATIONS 298 NUMERICAL INTEGRATION AND STATE TRANSITION
298 STATIC AND QUASISTATIC EQUILIBRIUM RESPONSE TO INPUTS 305 INITIAL
RESPONSE TO CONTROL INPUTS 310 CONTROLLABILITY AND OBSERVABILITY OF
MOTIONS 310 TRUNCATION AND RESIDUALIZATION 314 4.3 STABILITY AND MODES
OF MOTION 315 STABILITY OF TRANSIENT RESPONSE 316 FOURIER AND LAPLACE
TRANSFORMS 321 MODES OF AIRCRAFT MOTION 329 PHASE PLANE 338 4.4
FREQUENCY-DOMAIN ANALYSIS 342 TRANSFER FUNCTIONS AND FREQUENCY RESPONSE
342 NYQUIST PLOT AND NICHOLS CHART 355 ROOT LOCUS 357 4.5 DEALING WITH
UNCERTAINTY 361 RANDOM VARIABLES AND PROCESSES 363 DYNAMIC RESPONSE TO
RANDOM INPUTS AND INITIAL CONDITIONS 367 EFFECTS OF SYSTEM PARAMETER
VARIATIONS 372 SYSTEM SURVEY 373 MONTE CARLO EVALUATION 375 STOCHASTIC
ROOT LOCUS 378 4.6 LINEAR AEROELASTICITY 385 STRESS, STRAIN, AND
MATERIAL PROPERTIES 388 MONOCOQUE AND SEMIMONOCOQUE STRUCTURES 389 FORCE
AND MOMENTS ON A SIMPLE BEAM 391 STATIC DEFLECTION OF A SIMPLE BEAM
UNDER LOAD 394 VIBRATIONS OF A SIMPLE BEAM 396 CONTENTS XI COUPLED
VIBRATIONS OF AN ELASTICALLY RESTRAINED RIGID AIRFOIL 405 VIBRATIONS OF
A COMPLEX STRUCTURE 412 THE FOUR-BLOCK STRUCTURE 418 FUEL SLOSH 418 4.7
INTRODUCTION TO FLYING QUALITIES AND FLIGHT CONTROL SYSTEMS 419
COGNITIVE/BIOLOGICAL MODELS AND PILOTING ACTION 421 AIRCRAFT FLYING
QUALITIES 426 LINEAR-QUADRATIC REGULATOR 428 STEADY-STATE RESPONSE TO
COMMAND INPUT 432 IMPLICIT MODEL-FOLLOWING AND INTEGRAL COMPENSATION 434
OPTIMAL STATE ESTIMATION 438 LINEAR-QUADRATIC-GAUSSIAN REGULATOR 440
DESIGN FOR STOCHASTIC ROBUSTNESS 441 REFERENCES 443 CHAPTER FIVE
LONGITUDINAL MOTIONS 451 5.1 LONGITUDINAL EQUATIONS OF MOTION 452 5.2
REDUCED-ORDER MODELS OF LONG-PERIOD MODES 457 SECOND-ORDER PHUGOID-MODE
APPROXIMATION 457 EFFECTS OF COMPRESSIBILITY 473 EFFECTS OF ALTITUDE
VARIATION 476 EFFECTS OF WIND SHEAR 480 5.3 REDUCED-ORDER MODEL OF THE
SHORT-PERIOD MODE 482 SECOND-ORDER APPROXIMATION 483 EFFECTS OF
COMPRESSIBILITY AND HIGH ANGLE OF ATTACK 502 5.4 COUPLED
PHUGOID/SHORT-PERIOD DYNAMICS 503 RESIDUALIZED PHUGOID MODE 505
FOURTH-ORDER MODEL 507 LONGITUDINAL FLYING QUALITIES 525 5.5 CONTROL
MECHANISMS, STICK-FREE STABILITY, AND TRIM 533 ELEVATOR CONTROL
MECHANISM 534 SHORT-PERIOD/CONTROL-MECHANISM COUPLING 538 CONTROL FORCE
FOR TRIMMED FLIGHT 541 XII CONTENTS ELEVATOR ANGLE AND STICK FORCE PER G
545 TAIL-WAGS-DOG EFFECT 548 5.6 LONGITUDINAL AEROELASTIC EFFECTS 549
TRUNCATED AND RESIDUALIZED ELASTIC-BODY MODELS 550 COUPLING OF THE
SHORT-PERIOD WITH A SINGLE ELASTIC MODE 552 REFERENCES 569 CHAPTER SIX
LATERAL-DIRECTIONAL MOTIONS 573 6.1 LATERAL-DIRECTIONAL EQUATIONS OF
MOTION 574 6.2 REDUCED-ORDER MODEL OF THE DUTCH ROLL MODE 577 6.3
REDUCED-ORDER MODEL OF ROLL AND SPIRAL MODES 587 6.4 COUPLED
LATERAL-DIRECTIONAL DYNAMICS 595 A TRUNCATED DUTCH ROLL/ROLL MODEL 597
RESIDUALIZED LATERAL-DIRECTIONAL MODELS 598 FOURTH-ORDER MODEL 604
LATERAL-DIRECTIONAL FLYING QUALITIES 624 6.5 CONTROL MECHANISMS,
NONLINEARITY, AND TIME DELAY 629 RUDDER CONTROL MECHANISM 631 DUTCH
ROLL/RUDDER COUPLING 634 QUASILINEAR REPRESENTATION OF NONLINEARITY 646
QUASILINEAR ROOT LOCUS ANALYSIS 654 ROLL-SPIRAL/AILERON COUPLING 656
SPOILER NONLINEARITY AND TIME DELAY 660 6.6 LATERAL-DIRECTIONAL
AEROELASTIC EFFECTS 665 EQUILIBRIUM RESPONSE TO CONTROL 667 EIGENVALUES
AND ROOT LOCUS ANALYSIS OF PARAMETER VARIATIONS 668 RESPONSE TO INITIAL
CONDITIONS AND STEP CONTROL INPUTS 672 REFERENCES 678 CHAPTER SEVEN
COUPLED LONGITUDINAL AND LATERAL-DIRECTIONAL MOTIONS 681 7.1
SMALL-AMPLITUDE MOTIONS 682 EFFECTS OF ROTATING MACHINERY 685 ASYMMETRIC
INERTIAL AND AERODYNAMIC PROPERTIES 690 ASYMMETRIC FLIGHT CONDITION AND
CONSTANT ANGULAR RATE 695 COUPLING CONTROLS 704 CONTENTS XIII 7.2
INERTIAL COUPLING OF PITCH AND YAW MOTIONS 705 FIFTH-ORDER MODEL OF
COUPLED DYNAMICS 705 TRUNCATED AND RESIDUALIZED FOURTH-ORDER MODELS 712
RESPONSE TO CONTROLS DURING STEADY ROLLING 725 7.3 MULTIPLE EQUILIBRIUM
POINTS 728 SECOND-ORDER EXAMPLES OF MULTIPLE EQUILIBRIA 728 EFFECTS OF
CROSS-COUPLING AND CONTROL ON ROLLING EQUILIBRIUM 736 7.4 FLIGHT AT HIGH
ANGLE OF ATTACK 748 HIGH-ANGLE-OF-ATTACK AERODYNAMICS AND CONTROL
EFFECTS 749 FULLY DEVELOPED SPINS 767 SIMULATED MOTIONS OF A BUSINESS
JET AIRCRAFT 771 STABILITY OF HIGH-ANGLE-OF-ATTACK MANEUVERS 774
PILOT-AIRCRAFT INTERACTIONS 777 GAIN-SCHEDULED STABILITY AND COMMAND
AUGMENTATION 783 ADAPTIVE NEURAL NETWORK CONTROL 785 ROBUST
NONLINEAR-INVERSE-DYNAMIC CONTROL 789 REFERENCE 791 CHAPTER EIGHT
EPILOGUE 803 APPENDIX A CONSTANTS, UNITS, AND CONVERSION FACTORS 807
REFERENCES 809 APPENDIX B MATHEMATICAL MODEL AND SIX-DEGREE-OF-FREEDOM
SIMULATION OF A BUSINESS JET AIRCRAFT 810 B.I MAIN PROGRAM FOR ANALYSIS
AND SIMULATION (FLIGHT) 811 B.2 LOW-ANGLE-OF-ATTACK, MACH-DEPENDENT
MODEL (LOAEROMODEL) 811 B.3 HIGH-ANGLE-OF-ATTACK, LOW-SUBSONIC MODEL
(HIAEROMODEL) 811 B.4 SUPPORTING FUNCTIONS 812 B.4.1 EQUATIONS OF MOTION
(EOM) 812 XIV CONTENTS B.4.2 COST FUNCTION FOR AERODYNAMIC TRIM
(TRIMCOST) 812 B.4.3 DIRECTION COSINE MATRIX (DCM) 813 B.4.4 LINEAR
SYSTEM MATRICES (LINMODEL) 813 B.4.5 WIND FIELD (WINDFIELD) 813 B.4.6
ATMOSPHERIC STATE (ATMOS) 813 REFERENCE 813 APPENDIX C LINEAR SYSTEM
SURVEY 814 C.I MAIN PROGRAM FOR ANALYSIS AND SIMULATION (SURVEY) 814 C.2
SUPPORTING FUNCTIONS 815 C.2.1 REDUCED-ORDER MODELS (LONLATDIR) 815
C.2.2 TRANSIENT RESPONSE (TRANS) 815 C.2.3 STATIC RESPONSE (STATIC) 815
C.2.4 CONTROLLABILITY AND OBSERVABILITY (CONOBS) 815 C.2.5 NATURAL
FREQUENCY (NATFREQ) 815 C.2.6 STABILITY AND MODES OF MOTION (STABMODE)
815 APPENDIX D PAPER AIRPLANE PROGRAM 816 APPENDIX E BIBLIOGRAPHY OF
NASA REPORTS RELATED TO AIRCRAFT CONFIGURATION AERODYNAMICS 818
AEROSERVOELASTICITY 818 COMPONENT AERODYNAMICS 819 : CONFIGURATION
AERODYNAMICS 819 CONTROL EFFECTS 825 FLYING QUALITIES 826 NUMERICAL
METHODS 826 REENTRY VEHICLES 827 SPIN AND STALL AERODYNAMICS 828
TURBULENCE EFFECTS 829 INDEX 831
|
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| id | DE-604.BV019656901 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T20:02:18Z |
| institution | BVB |
| isbn | 0691114072 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-012985403 |
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| physical | XVIII, 845 S. graph. Darst. |
| publishDate | 2004 |
| publishDateSearch | 2004 |
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| publisher | Princeton Univ. Pr. |
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| spelling | Stengel, Robert F. 1938- Verfasser (DE-588)1274486580 aut Flight dynamics Robert F. Stengel Princeton, NJ [u.a.] Princeton Univ. Pr. 2004 XVIII, 845 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Aerodynamics Airplanes Performance Flight Flugmechanik (DE-588)4154760-3 gnd rswk-swf Flugmechanik (DE-588)4154760-3 s DE-604 HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=012985403&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Stengel, Robert F. 1938- Flight dynamics Aerodynamics Airplanes Performance Flight Flugmechanik (DE-588)4154760-3 gnd |
| subject_GND | (DE-588)4154760-3 |
| title | Flight dynamics |
| title_auth | Flight dynamics |
| title_exact_search | Flight dynamics |
| title_full | Flight dynamics Robert F. Stengel |
| title_fullStr | Flight dynamics Robert F. Stengel |
| title_full_unstemmed | Flight dynamics Robert F. Stengel |
| title_short | Flight dynamics |
| title_sort | flight dynamics |
| topic | Aerodynamics Airplanes Performance Flight Flugmechanik (DE-588)4154760-3 gnd |
| topic_facet | Aerodynamics Airplanes Performance Flight Flugmechanik |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=012985403&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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