Dynamics of flight: stability and control
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| Main Authors: | , |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
New York, NY [u.a.]
Wiley
1996
|
| Edition: | 3. ed. |
| Subjects: | |
| Online Access: | Inhaltsverzeichnis |
| Item Description: | Literaturangaben |
| Physical Description: | XI, 382 S. graph. Darst. |
| ISBN: | 0471034185 9780471034186 |
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| 245 | 1 | 0 | |a Dynamics of flight |b stability and control |c Bernard Etkin; Lloyd Duff Reid |
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Record in the Search Index
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|---|---|
| adam_text | T H I R D E D I T I O N DYNAMICS OF FLIGHT STABILITY AND CONTROL BERNARD
ETKIN UNIVERSITY PROFESSOR EMERITUS INSTITUTE FOR AEROSPACE STUDIES
UNIVERSITY OF TORONTO LLOYD DUFF REID PROFESSOR INSTITUTE FOR AEROSPACE
STUDIES UNIVERSITY OF TORONTO JOHN WILEY & SONS, INC. CONTENTS CHAPTER L
INTRODUCTION 1.1 THE SUBJECT MATTER OF DYNAMICS OF FLIGHT 1 1.2 THE
TOOLS OF FLIGHT DYNAMICISTS 5 1.3 STABILITY, CONTROL, AND EQUILIBRIUM 6
1.4 THE HUMAN PILOT 8 1.5 HANDLING QUALITIES REQUIREMENTS 11 1.6 AXES
AND NOTATION 15 CHAPTER 2 STATIC STABILITY AND CONTROL * PART 1 2.1
GENERAL REMARKS 18 2.2 SYNTHESIS OF LIFT AND PITCHING MOMENT 23 2.3
TOTAL PITCHING MOMENT AND NEUTRAL POINT 29 2.4 LONGITUDINAL CONTROL 33
2.5 THE CONTROL HINGE MOMENT 41 2.6 INFLUENCE OF A FREE ELEVATOR ON LIFT
AND MOMENT 44 2.7 THE USE OF TABS 47 2.8 CONTROL FORCE TO TRIM 48 2.9
CONTROL FORCE GRADIENT 51 2.10 EXERCISES 52 2.11 ADDITIONAL SYMBOLS
INTRODUCED IN CHAPTER 2 57 CHAPTER 3 STATIC STABILITY AND CONTROL * PART
2 3.1 MANEUVERABILITY-ELEVATOR ANGLE PER G 60 3.2 CONTROL FORCE PER G 63
3.3 INFLUENCE OF HIGH-LIFT DEVICES ON TRIM AND PITCH STIFFNESS 64 3.4
INFLUENCE OF THE PROPULSIVE SYSTEM ON TRIM AND PITCH STIFFNESS 66 3.5
EFFECT OF STRUCTURAL FLEXIBILITY 72 3.6 GROUND EFFECT 74 3.7 CG LIMITS
74 3.8 LATERAL AERODYNAMICS 76 3.9 WEATHERCOCK STABILITY (YAW STIFFNESS)
77 3.10 YAW CONTROL 80 3.11 ROLL STIFFNESS 81 3.12 THE DERIVATIVE C LP
83 3.13 ROLL CONTROL 86 3.14 EXERCISES 89 3.15 ADDITIONAL SYMBOLS
INTRODUCED IN CHAPTER 3 91 CHAPTER 4 GENERAL EQUATIONS OF UNSTEADY
MOTION 4.1 GENERAL REMARKS 93 4.2 THE RIGID-BODY EQUATIONS 93 X CONTENTS
4.3 EVALUATION OF THE ANGULAR MOMENTUM H 96 4.4 ORIENTATION AND POSITION
OF THE AIRPLANE 98 4.5 EULER S EQUATIONS OF MOTION 100 4.6 EFFECT OF
SPINNING ROTORS ON THE EULER EQUATIONS 103 4.7 THE EQUATIONS COLLECTED
103 4.8 DISCUSSION OF THE EQUATIONS 104 4.9 THE SMALL-DISTURBANCE THEORY
107 4.10 THE NONDIMENSIONAL SYSTEM 115 4.11 DIMENSIONAL STABILITY
DERIVATIVES 118 4.12 ELASTIC DEGREES OF FREEDOM 120 4.13 EXERCISES 126
4.14 ADDITIONAL SYMBOLS INTRODUCED IN CHAPTER 4 127 CHAPTER 5 THE
STABILITY DERIVATIVES 5.1 GENERAL REMARKS 129 5.2 THE A DERIVATIVES 129
5.3 THE U DERIVATIVES 131 5.4 THE Q DERIVATIVES 135 5.5 THE A
DERIVATIVES 141 5.6 THE J8 DERIVATIVES 148 5.7 THE P DERIVATIVES 149 5.8
THE R DERIVATIVES 153 5.9 SUMMARY OF THE FORMULAS 154 5.10 AEROELASTIC
DERIVATIVES 156 5.11 EXERCISES 159 5.12 ADDITIONAL SYMBOLS INTRODUCED IN
CHAPTER 5 160 CHAPTER 6 STABILITY OF UNCONTROLLED MOTION 6.1 FORM OF
SOLUTION OF SMALL-DISTURBANCE EQUATIONS 161 6.2 LONGITUDINAL MODES OF A
JET TRANSPORT 165 6.3 APPROXIMATE EQUATIONS FOR THE LONGITUDINAL MODES
171 6.4 GENERAL THEORY OF STATIC LONGITUDINAL STABILITY 175 6.5 EFFECT
OF RIGHT CONDITION ON THE LONGITUDINAL MODES OF A SUBSONIC JET TRANSPORT
177 6.6 LONGITUDINAL CHARACTERISTICS OF A STOL AIRPLANE 184 6.7 LATERAL
MODES OF A JET TRANSPORT 187 6.8 APPROXIMATE EQUATIONS FOR THE LATERAL
MODES 193 6.9 EFFECTS OF WIND 196 6.10 EXERCISES 201 6.11 ADDITIONAL
SYMBOLS INTRODUCED IN CHAPTER 6 203 CHAPTER 7 RESPONSE TO ACTUATION OF
THE CONTROLS * OPEN LOOP 7.1 GENERAL REMARKS 204 7.2 RESPONSE OF
LINEAR/INVARIANT SYSTEMS 207 7.3 IMPULSE RESPONSE 210 CONTENTS XI 7.4
STEP-FUNCTION RESPONSE 213 7.5 FREQUENCY RESPONSE 214 7.6 LONGITUDINAL
RESPONSE 228 7.7 RESPONSES TO ELEVATOR AND THROTTLE 229 7.8 LATERAL
STEADY STATES 237 7.9 LATERAL FREQUENCY RESPONSE 243 7.10 APPROXIMATE
LATERAL TRANSFER FUNCTIONS 247 7.11 TRANSIENT RESPONSE TO AILERON AND
RUDDER 252 7.12 INERTIAL COUPLING IN RAPID MANEUVERS 256 7.13 EXERCISES
256 7.14 ADDITIONAL SYMBOLS INTRODUCED IN CHAPTER 7 258 CHAPTER 8
CLOSED-LOOP CONTROL 8.1 GENERAL REMARKS 259 8.2 STABILITY OF CLOSED LOOP
SYSTEMS 264 8.3 PHUGOID SUPPRESSION: PITCH ATTITUDE CONTROLLER 266 8.4
SPEED CONTROLLER 270 8.5 ALTITUDE AND GLIDE PATH CONTROL 275 8.6 LATERAL
CONTROL 280 8.7 YAW DAMPER 287 8.8 ROLL CONTROLLER 290 8.9 GUST
ALLEVIATION 295 8.10 EXERCISES 300 8.11 ADDITIONAL SYMBOLS INTRODUCED IN
CHAPTER 8 301 APPENDIX A ANALYTICAL TOOLS A.I LINEAR ALGEBRA 303 A.2 THE
LAPLACE TRANSFORM 304 A.3 THE CONVOLUTION INTEGRAL 309 A.4 COORDINATE
TRANSFORMATIONS 310 A.5 COMPUTATION OF EIGENVALUES AND EIGENVECTORS 315
A.6 VELOCITY AND ACCELERATION IN AN ARBITRARILY MOVING FRAME 316
APPENDIX B DATA FOR ESTIMATING AERODYNAMIC DERIVATIVES 319 APPENDIX C
MEAN AERODYNAMIC CHORD, MEAN AERODYNAMIC CENTER, AND CM ACW 357 APPENDIX
D THE STANDARD ATMOSPHERE AND OTHER DATA 364 APPENDIX E DATA FOR THE
BOEING 747-100 369 REFERENCES 372 INDEX YII
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| indexdate | 2024-07-09T17:59:16Z |
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| isbn | 0471034185 9780471034186 |
| language | English |
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| physical | XI, 382 S. graph. Darst. |
| publishDate | 1996 |
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| publisher | Wiley |
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| spelling | Etkin, Bernard Verfasser aut Dynamics of flight stability and control Bernard Etkin; Lloyd Duff Reid 3. ed. New York, NY [u.a.] Wiley 1996 XI, 382 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Literaturangaben Avions - Stabilité Aérodynamique Stabiliteit gtt Vliegtuigen gtt Aerodynamics Stability of airplanes Flugmechanik (DE-588)4154760-3 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf Flugkörper (DE-588)4154756-1 gnd rswk-swf Flugmechanik (DE-588)4154760-3 s DE-604 Flugkörper (DE-588)4154756-1 s Aerodynamik (DE-588)4000589-6 s Reid, Lloyd Duff Verfasser aut HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=007221344&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Etkin, Bernard Reid, Lloyd Duff Dynamics of flight stability and control Avions - Stabilité Aérodynamique Stabiliteit gtt Vliegtuigen gtt Aerodynamics Stability of airplanes Flugmechanik (DE-588)4154760-3 gnd Aerodynamik (DE-588)4000589-6 gnd Flugkörper (DE-588)4154756-1 gnd |
| subject_GND | (DE-588)4154760-3 (DE-588)4000589-6 (DE-588)4154756-1 |
| title | Dynamics of flight stability and control |
| title_auth | Dynamics of flight stability and control |
| title_exact_search | Dynamics of flight stability and control |
| title_full | Dynamics of flight stability and control Bernard Etkin; Lloyd Duff Reid |
| title_fullStr | Dynamics of flight stability and control Bernard Etkin; Lloyd Duff Reid |
| title_full_unstemmed | Dynamics of flight stability and control Bernard Etkin; Lloyd Duff Reid |
| title_short | Dynamics of flight |
| title_sort | dynamics of flight stability and control |
| title_sub | stability and control |
| topic | Avions - Stabilité Aérodynamique Stabiliteit gtt Vliegtuigen gtt Aerodynamics Stability of airplanes Flugmechanik (DE-588)4154760-3 gnd Aerodynamik (DE-588)4000589-6 gnd Flugkörper (DE-588)4154756-1 gnd |
| topic_facet | Avions - Stabilité Aérodynamique Stabiliteit Vliegtuigen Aerodynamics Stability of airplanes Flugmechanik Aerodynamik Flugkörper |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=007221344&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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