Flight performance of fixed and rotary wing aircraft:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Amsterdam [u.a.]
Elsevier
2006
|
| Ausgabe: | 1. ed. |
| Schriftenreihe: | Elsevier aerospace engineering series
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XXVII, 565 S. Ill., graph. Darst. |
| ISBN: | 0750668172 9780750668170 |
Internformat
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| 100 | 1 | |a Filippone, Antonio |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Flight performance of fixed and rotary wing aircraft |c Antonio Filippone |
| 250 | |a 1. ed. | ||
| 264 | 1 | |a Amsterdam [u.a.] |b Elsevier |c 2006 | |
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| 650 | 4 | |a Airplanes |x Performance | |
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Datensatz im Suchindex
| _version_ | 1804135636950581248 |
|---|---|
| adam_text | FLIGHT PERFORMANCE OF FIXED AND ROTARY WING AIRCRAFT ANTONIO FILIPPONE
*~ IFEFI AMSTERDAM * BOSTON * HEIDELBERG * LONDON * NEW YORK * OXFORD J
^ I L E PARIS * SAN DIEGO * SAN FRANCISCO * SINGAPORE * SYDNEY * TOKYO
ELSEVIER BUTTERWORTH-HEINEMANN IS AN IMPRINT OF ELSEVIER CONTENTS
PREFACE XI ACKNOWLEDGMENTS XV LIST OF TABLES XVII NOMENCLATURE:
ORGANIZATIONS XIX NOMENCLATURE: ACRONYMS XX NOMENCLATURE: MAIN SYMBOLS
XXII NOMENCLATURE: GREEK SYMBOLS XXV NOMENCLATURE:
SUBSCRIPTS/SUPERSCRIPTS XXVI SUPPLEMENTS TO THE TEXT XXVII PART I
FIXED-WING AIRCRAFT PERFORMANCE 1 INTRODUCTION 3 1.1 PHYSICAL UNITS USED
4 1.2 PERFORMANCE PARAMETERS 5 1.3 PERFORMANCE OPTIMIZATION 7 1.4
CERTIFICATE OF AIRWORTHINESS 7 1.5 UPGRADING OF AIRCRAFT PERFORMANCE 8
1.6 MISSION PROFILES 9 PROBLEMS 13 2 THE AIRCRAFT AND ITS ENVIRONMENT 15
2.1 GENERAL AIRCRAFT MODEL 15 2.2 REFERENCE SYSTEMS 17 2.3 FORCES ON THE
AIRCRAFT 20 2.4 MOMENTS OF INERTIA 21 2.5 FLIGHT DYNAMICS EQUATIONS 22
2.6 THE INTERNATIONAL STANDARD ATMOSPHERE 23 2.7 NON-STANDARD CONDITIONS
28 PROBLEMS 30 3 WEIGHT PERFORMANCE 33 3 . 1 THE AIRCRAFT S WEIGHT 33
3.2 DEFINITION OF WEIGHTS 40 3.3 WEIGHT ESTIMATION 42 VI CONTENTS 3.4
WEIGHT MANAGEMENT 42 3.5 RANGE/PAY LOAD DIAGRAM 44 3.6 DIRECT OPERATING
COSTS 46 PROBLEMS 47 4 AERODYNAMIC PERFORMANCE 49 4.1 AERODYNAMIC FORCES
49 4.2 LIFT EQUATION 51 4.3 VORTEX LIFT 52 4.4 HIGH-LIFT SYSTEMS 55 4.5
DRAG EQUATION 57 4.6 GLIDE RATIO 61 4.7 GLIDE RATIO AT TRANSONIC AND
SUPERSONIC SPEED 63 4.8 PRACTICAL ESTIMATION OF THE DRAG COEFFICIENT 65
4.9 COMPRESSIBILITY EFFECTS 66 4.10 TRANSONIC DRAG RISE 67 4.11 LIFT AND
TRANSONIC BUFFET 68 4.12 AERO-THERMODYNAMIC HEATING 69 4.13 AERODYNAMIC
PENETRATION AND RADIUS 71 4.14 AIRCRAFT VORTEX WAKES 72 4.15
AERODYNAMICS AND PERFORMANCE 74 PROBLEMS 75 5 ENGINE PERFORMANCE 77 5.1
GAS TURBINE ENGINES 77 81 83 84 86 88 93 94 95 108 111 111 112 113 117
117 119 119 121 124 126 128 5.2 5.3 5.4 5.5 5.6 5.7 5.8 5.9 INTERNAL
COMBUSTION ENGINES ENGINE FLIGHT ENVELOPES POWER AND THRUST DEFINITIONS
GENERALIZED ENGINE PERFORMANCE FUEL FLOW PROPULSIVE EFFICIENCY THRUST
CHARACTERISTICS PROPELLER CHARACTERISTICS PROBLEMS FLIGHT ENVELOPES 6.1
6.2 6.3 6.4 6.5 6.6 6.7 6.8 6.9 6.10 6.11 GENERAL DEFINITIONS AIRCRAFT
SPEED RANGE DEFINITION OF SPEEDS STEADY STATE LEVEL FLIGHT SPEED IN
LEVEL FLIGHT ABSOLUTE CEILING OF JET AIRCRAFT ABSOLUTE CEILING OF
PROPELLER AIRCRAFT OPTIMAL SPEEDS FOR LEVEL FLIGHT GENERAL FLIGHT
ENVELOPES LIMITING FACTORS ON FLIGHT ENVELOPES DASH SPEED OF SUPERSONIC
AIRCRAFT 6.12 6.13 ABSOLUTE CEILING OF SUPERSONIC AIRCRAFT SUPERSONIC
ACCELERATION PROBLEMS 7 TAKE-OFF AND LANDING 7.1 7.2 7.3 7.4 7.5 7.6 7.7
7.8 7.9 7.10 7.11 7.12 7.13 7.14 DEFINITION OF TERMINAL PHASES
CONVENTIONAL TAKE-OFF GROUND RUN OF JET AIRCRAFT SOLUTIONS OF THE
TAKE-OFF EQUATION ROTATION AND INITIAL CLIMB TAKE-OFF WITH ONE ENGINE
INOPERATIVE CALCULATION OF THE BALANCED FIELD LENGTH GROUND RUN OF
PROPELLER AIRCRAFT WAT CHARTS MISSED TAKE-OFF FINAL APPROACH AND LANDING
LANDING RUN EFFECTS OF THE WIND GROUND MANEUVERING PROBLEMS 8 CLIMB AND
GLIDING 8.1 8.2 8.3 8.4 8.5 8.6 8.7 8.8 8.9 8.10 8.11 8.12 8.13 8.14
GOVERNING EQUATIONS RATE OF CLIMB STEADY CLIMB OF PROPELLER AIRPLANE
CLIMB OF JET AIRPLANE POLAR DIAGRAM FOR RATE OF CLIMB ENERGY METHODS
SPECIFIC EXCESS POWER DIAGRAMS DIFFERENTIAL EXCESS POWER PLOTS MINIMUM
PROBLEMS WITH ENERGY METHOD STEADY STATE GLIDING GENERAL GLIDING FLIGHT
MAXIMUM GLIDE RANGE WITH ENERGY METHOD MINIMUM FLIGHT PATHS ADDITIONAL
RESEARCH ON AIRCRAFT CLIMB PROBLEMS 9 CRUISE PERFORMANCE 9.1 9.2 9.3 9.4
9.5 9.6 9.7 9.8 IMPORTANCE OF THE CRUISE FLIGHT GENERAL DEFINITIONS
POINT PERFORMANCE THE BREGUET RANGE EQUATION SUBSONIC CRUISE OF JET
AIRCRAFT MISSION FUEL CRUISE WITH INTERMEDIATE STOP AIRCRAFT SELECTION
CONTENTS VII 131 131 135 137 137 139 141 143 148 150 151 153 154 155 156
157 161 161 161 165 165 166 167 175 179 181 183 184 186 190 194 196 198
201 202 205 205 206 206 216 218 224 230 232 VIII CONTENTS 9.9 SUPERSONIC
CRUISE 233 9.10 CRUISE RANGE OF PROPELLER AIRCRAFT 237 9.11 ENDURANCE
238 9.12 EFFECT OF WEIGHT ON CRUISE RANGE 239 9.13 EFFECT OF THE WIND ON
CRUISE RANGE 239 9.14 ADDITIONAL RESEARCH ON AIRCRAFT CRUISE 241 9.15
FORMATION FLIGHT 241 PROBLEMS 248 10 MANEUVER PERFORMANCE 251 10.1
BANKED LEVEL TURNS 251 10.2 BANKED TURN AT CONSTANT THRUST 253 10.3
POWER REQUIREMENTS 255 10.4 EFFECT OF WEIGHT ON TURN RADIUS 256 10.5
MANEUVER ENVELOPE: N-V DIAGRAM 257 10.6 TURN RATES 259 10.7 SUSTAINABLE
G-LOADS 262 10.8 UNPOWERED TURN 264 10.9 SOARING FLIGHT 265 10.10 ROLL
PERFORMANCE 271 10.11 AIRCRAFT CONTROL UNDER THRUST ASYMMETRY 283 10.12
PULL-UP MANEUVER AND THE LOOP 287 10.13 ZERO-GRAVITY ATMOSPHERIC FLIGHT
289 10.14 FLIGHT PATH TO A MOVING TARGET 295 PROBLEMS 297 PART II
ROTARY-WING AIRCRAFT PERFORMANCE 11 ROTORCRAFT PERFORMANCE 301 301 302
305 306 307 311 312 313 11.1 11.2 11.3 11.4 11.5 11.6 11.7 FUNDAMENTALS
HELICOPTER CONFIGURATIONS MISSION PROFILES FLIGHT ENVELOPES DEFINITIONS
AND REFERENCE SYSTEMS NON-DIMENSIONAL PARAMETERS METHODS FOR PERFORMANCE
CALCULATIONS PROBLEMS ROTORCRAFT IN VERTICAL FLIGHT 12.1 12.2 12.3 12.4
12.5 12.6- 12.7 12.8 HOVER PERFORMANCE EFFECT OF BLADE TWIST
NON-DIMENSIONAL HOVER PERFORMANCE VERTICAL CLIMB CEILING PERFORMANCE
GROUND EFFECT VERTICAL DESCENT HOVER ENDURANCE 12 ROTORCRAFT IN VERTICAL
FLIGHT 315 315 323 324 326 328 331 332 334 PROBLEMS 335 CONTENTS IX 13
ROTORCRAFT IN FORWARD FLIGHT 337 13.1 ASYMMETRY OF ROTOR LOADS 337 13.2
POWER REQUIREMENTS 338 13.3 ROTOR DISK ANGLE 357 13.4 CALCULATION OF
FORWARD FLIGHT POWER 359 13.5 L/D OF THE HELICOPTER 3 61 13.6 FORWARD
FLIGHT ANALYSIS 362 13.7 PROPULSIVE EFFICIENCY 366 13.8 CLIMB
PERFORMANCE 367 13.9 PERFORMANCE OF TANDEM HELICOPTERS 370 13.10 SINGLE
OR TANDEM HELICOPTER? 377 PROBLEMS 380 14 ROTORCRAFT MANEUVER 383 14.1
LIMITS ON FLIGHT ENVELOPES 383 14.2 KINETIC ENERGY OF THE ROTOR 385 14.3
AUTOROTATIVE INDEX 387 14.4 AUTOROTATIVE PERFORMANCE 389 14.5
HEIGHT/VELOCITY DIAGRAM 398 14.6 THE VORTEX RING STATE 400 14.7 TAKE-OFF
AND LANDING 404 14.8 TURN PERFORMANCE 404 14.9 POWER REQUIRED FOR
TURNING 406 14.10 MORE ON TAIL ROTOR PERFORMANCE 410 PROBLEMS 412 15
ROTORCRAFT MISSION ANALYSIS 413 15.1 SPECIFIC AIR RANGE 413 15.2
NON-DIMENSIONAL ANALYSIS OF THE SAR 415 15.3 ENDURANCE AND SPECIFIC
ENDURANCE 416 15.4 SPEED FOR MINIMUM POWER 417 15.5 SPEED FOR MAXIMUM
RANGE 419 15.6 FUEL TO CLIMB 420 15.7 PAYLOAD/RANGE DIAGRAM 422 15.8
COMPARATIVE PAYLOAD FRACTION 428 15.9 MISSION ANALYSIS 429 PROBLEMS ^
430 PART III V/STOL AND NOISE PERFORMANCE 16 V/STOL PERFORMANCE 435 16.1
HOVER CHARACTERISTICS 435 16.2. JET-INDUCED LIFT 437 16.3 LIFT
AUGMENTATION 440 16.4 CALCULATION OF SHORT TAKE-OFF 441 16.5 SKI JUMP
445 X CONTENTS 16.6 CONVERTIPLANES OR TILT ROTORS 448 16.7 V/STOL FLIGHT
ENVELOPES 449 PROBLEMS 449 17 NOISE PERFORMANCE 451 17.1 DEFINITIONS OF
SOUND AND NOISE 452 17.2 TRENDS IN NOISE REDUCTION 454 17.3 AIRFRAME
NOISE OF FIXED-WING AIRCRAFT 456 17.4 ENGINE NOISE 460 17.5 NOISE
CERTIFICATION PROCEDURE 461 17.6 NOISE REDUCTION FROM OPERATIONS 464
17.7 MINIMUM NOISE TO CLIMB 467 17.8 HELICOPTER NOISE 469 17.9
HELICOPTER NOISE REDUCTION 472 17.10 NOISE CERTIFICATION OF CIVIL
HELICOPTERS 472 17.11 SONIC BOOM 473 PROBLEMS 478 APPENDIX A AIRCRAFT
MODELS 479 A. 1 AIRCRAFT A: SUBSONIC COMMERCIAL JET 479 A.2 AIRCRAFT B:
TURBOPROP TRANSPORT AIRCRAFT 484 A.3 AIRCRAFT C: SUPERSONIC JET FIGHTER
487 A.4 AIRCRAFT D: GENERAL UTILITY HELICOPTER 494 A.5 AIRCRAFT E:
TANDEM HELICOPTER 502 APPENDIX B NOISE DATA 507 APPENDIX C SELECTED
SIMULATION PROGRAMS 509 C. 1 ASSEMBLING AIRCRAFT FORCES 509 C.2
CALCULATION OF NUMERICAL DERIVATIVES 510 C.3 OPTIMAL CLIMB OF FIGHTER
JET AIRCRAFT 510 C.4 OPTIMAL CLIMB RATE OF TURBOPROP 513 C.5 CALCULATION
OF MISSION FUEL 515 C.6 SUPERSONIC ACCELERATION 518 C.7 ASYMMETRIC
THRUST CONTROL 521 C.8 HOVER POWER WITH BLADE ELEMENT THEORY 524 C.9
FORWARD FLIGHT POWER OF HELICOPTER 526 BIBLIOGRAPHY 531 INDEX 553
|
| adam_txt |
FLIGHT PERFORMANCE OF FIXED AND ROTARY WING AIRCRAFT ANTONIO FILIPPONE
*~ "IFEFI AMSTERDAM * BOSTON * HEIDELBERG * LONDON * NEW YORK * OXFORD J
^ I L E PARIS * SAN DIEGO * SAN FRANCISCO * SINGAPORE * SYDNEY * TOKYO
ELSEVIER BUTTERWORTH-HEINEMANN IS AN IMPRINT OF ELSEVIER CONTENTS
PREFACE XI ACKNOWLEDGMENTS XV LIST OF TABLES XVII NOMENCLATURE:
ORGANIZATIONS XIX NOMENCLATURE: ACRONYMS XX NOMENCLATURE: MAIN SYMBOLS
XXII NOMENCLATURE: GREEK SYMBOLS XXV NOMENCLATURE:
SUBSCRIPTS/SUPERSCRIPTS XXVI SUPPLEMENTS TO THE TEXT XXVII PART I
FIXED-WING AIRCRAFT PERFORMANCE 1 INTRODUCTION 3 1.1 PHYSICAL UNITS USED
4 1.2 PERFORMANCE PARAMETERS 5 1.3 PERFORMANCE OPTIMIZATION 7 1.4
CERTIFICATE OF AIRWORTHINESS 7 1.5 UPGRADING OF AIRCRAFT PERFORMANCE 8
1.6 MISSION PROFILES 9 PROBLEMS 13 2 THE AIRCRAFT AND ITS ENVIRONMENT 15
2.1 GENERAL AIRCRAFT MODEL 15 2.2 REFERENCE SYSTEMS 17 2.3 FORCES ON THE
AIRCRAFT 20 2.4 MOMENTS OF INERTIA 21 2.5 FLIGHT DYNAMICS EQUATIONS 22
2.6 THE INTERNATIONAL STANDARD ATMOSPHERE 23 2.7 NON-STANDARD CONDITIONS
28 PROBLEMS 30 3 WEIGHT PERFORMANCE 33 3". 1 THE AIRCRAFT'S WEIGHT 33
3.2 DEFINITION OF WEIGHTS 40 3.3 WEIGHT ESTIMATION 42 VI CONTENTS 3.4
WEIGHT MANAGEMENT 42 3.5 RANGE/PAY LOAD DIAGRAM 44 3.6 DIRECT OPERATING
COSTS 46 PROBLEMS 47 4 AERODYNAMIC PERFORMANCE 49 4.1 AERODYNAMIC FORCES
49 4.2 LIFT EQUATION 51 4.3 VORTEX LIFT 52 4.4 HIGH-LIFT SYSTEMS 55 4.5
DRAG EQUATION 57 4.6 GLIDE RATIO 61 4.7 GLIDE RATIO AT TRANSONIC AND
SUPERSONIC SPEED 63 4.8 PRACTICAL ESTIMATION OF THE DRAG COEFFICIENT 65
4.9 COMPRESSIBILITY EFFECTS 66 4.10 TRANSONIC DRAG RISE 67 4.11 LIFT AND
TRANSONIC BUFFET 68 4.12 AERO-THERMODYNAMIC HEATING 69 4.13 AERODYNAMIC
PENETRATION AND RADIUS 71 4.14 AIRCRAFT VORTEX WAKES 72 4.15
AERODYNAMICS AND PERFORMANCE 74 PROBLEMS 75 5 ENGINE PERFORMANCE 77 5.1
GAS TURBINE ENGINES 77 81 83 84 86 88 93 94 95 108 111 111 112 113 117
117 119 119 121 124 126 128 5.2 5.3 5.4 5.5 5.6 5.7 5.8 5.9 INTERNAL
COMBUSTION ENGINES ENGINE FLIGHT ENVELOPES POWER AND THRUST DEFINITIONS
GENERALIZED ENGINE PERFORMANCE FUEL FLOW PROPULSIVE EFFICIENCY THRUST
CHARACTERISTICS PROPELLER CHARACTERISTICS PROBLEMS FLIGHT ENVELOPES 6.1
6.2 6.3 6.4 6.5 6.6 6.7 6.8 6.9'" 6.10 6.11 GENERAL DEFINITIONS AIRCRAFT
SPEED RANGE DEFINITION OF SPEEDS STEADY STATE LEVEL FLIGHT SPEED IN
LEVEL FLIGHT ABSOLUTE CEILING OF JET AIRCRAFT ABSOLUTE CEILING OF
PROPELLER AIRCRAFT OPTIMAL SPEEDS FOR LEVEL FLIGHT GENERAL FLIGHT
ENVELOPES LIMITING FACTORS ON FLIGHT ENVELOPES DASH SPEED OF SUPERSONIC
AIRCRAFT 6.12 6.13 ABSOLUTE CEILING OF SUPERSONIC AIRCRAFT SUPERSONIC
ACCELERATION PROBLEMS 7 TAKE-OFF AND LANDING 7.1 7.2 7.3 7.4 7.5 7.6 7.7
7.8 7.9 7.10 7.11 7.12 7.13 7.14 DEFINITION OF TERMINAL PHASES
CONVENTIONAL TAKE-OFF GROUND RUN OF JET AIRCRAFT SOLUTIONS OF THE
TAKE-OFF EQUATION ROTATION AND INITIAL CLIMB TAKE-OFF WITH ONE ENGINE
INOPERATIVE CALCULATION OF THE BALANCED FIELD LENGTH GROUND RUN OF
PROPELLER AIRCRAFT WAT CHARTS MISSED TAKE-OFF FINAL APPROACH AND LANDING
LANDING RUN EFFECTS OF THE WIND GROUND MANEUVERING PROBLEMS 8 CLIMB AND
GLIDING 8.1 8.2 8.3 8.4 8.5 8.6 8.7 8.8 8.9 8.10 8.11 8.12 8.13 8.14
GOVERNING EQUATIONS RATE OF CLIMB STEADY CLIMB OF PROPELLER AIRPLANE
CLIMB OF JET AIRPLANE POLAR DIAGRAM FOR RATE OF CLIMB ENERGY METHODS
SPECIFIC EXCESS POWER DIAGRAMS DIFFERENTIAL EXCESS POWER PLOTS MINIMUM
PROBLEMS WITH ENERGY METHOD STEADY STATE GLIDING GENERAL GLIDING FLIGHT
MAXIMUM GLIDE RANGE WITH ENERGY METHOD MINIMUM FLIGHT PATHS ADDITIONAL
RESEARCH ON AIRCRAFT CLIMB PROBLEMS 9 CRUISE PERFORMANCE 9.1 9.2 9.3 9.4
9.5 9.6 9.7 9.8 IMPORTANCE OF THE CRUISE FLIGHT GENERAL DEFINITIONS
POINT PERFORMANCE THE BREGUET RANGE EQUATION SUBSONIC CRUISE OF JET
AIRCRAFT MISSION FUEL CRUISE WITH INTERMEDIATE STOP AIRCRAFT SELECTION
CONTENTS VII 131 131 135 137 137 139 141 143 148 150 151 153 154 155 156
157 161 161 161 165 165 166 167 175 179 181 183 184 186 190 194 196 198
201 202 205 205 206 206 216 218 224 230 232 VIII CONTENTS 9.9 SUPERSONIC
CRUISE 233 9.10 CRUISE RANGE OF PROPELLER AIRCRAFT 237 9.11 ENDURANCE
238 9.12 EFFECT OF WEIGHT ON CRUISE RANGE 239 9.13 EFFECT OF THE WIND ON
CRUISE RANGE 239 9.14 ADDITIONAL RESEARCH ON AIRCRAFT CRUISE 241 9.15
FORMATION FLIGHT 241 PROBLEMS 248 10 MANEUVER PERFORMANCE 251 10.1
BANKED LEVEL TURNS 251 10.2 BANKED TURN AT CONSTANT THRUST 253 10.3
POWER REQUIREMENTS 255 10.4 EFFECT OF WEIGHT ON TURN RADIUS 256 10.5
MANEUVER ENVELOPE: N-V DIAGRAM 257 10.6 TURN RATES 259 10.7 SUSTAINABLE
G-LOADS 262 10.8 UNPOWERED TURN 264 10.9 SOARING FLIGHT 265 10.10 ROLL
PERFORMANCE 271 10.11 AIRCRAFT CONTROL UNDER THRUST ASYMMETRY 283 10.12
PULL-UP MANEUVER AND THE LOOP 287 10.13 ZERO-GRAVITY ATMOSPHERIC FLIGHT
289 10.14 FLIGHT PATH TO A MOVING TARGET 295 PROBLEMS 297 PART II
ROTARY-WING AIRCRAFT PERFORMANCE 11 ROTORCRAFT PERFORMANCE 301 301 302
305 306 307 311 312 313 11.1 11.2 11.3 11.4 11.5 11.6 11.7 FUNDAMENTALS
HELICOPTER CONFIGURATIONS MISSION PROFILES FLIGHT ENVELOPES DEFINITIONS
AND REFERENCE SYSTEMS NON-DIMENSIONAL PARAMETERS METHODS FOR PERFORMANCE
CALCULATIONS PROBLEMS ROTORCRAFT IN VERTICAL FLIGHT 12.1 12.2 12.3 12.4
12.5 12.6- 12.7 12.8 HOVER PERFORMANCE EFFECT OF BLADE TWIST
NON-DIMENSIONAL HOVER PERFORMANCE VERTICAL CLIMB CEILING PERFORMANCE
GROUND EFFECT VERTICAL DESCENT HOVER ENDURANCE 12 ROTORCRAFT IN VERTICAL
FLIGHT 315 315 323 324 326 328 331 332 334 PROBLEMS 335 CONTENTS IX 13
ROTORCRAFT IN FORWARD FLIGHT 337 13.1 ASYMMETRY OF ROTOR LOADS 337 13.2
POWER REQUIREMENTS 338 13.3 ROTOR DISK ANGLE 357 13.4 CALCULATION OF
FORWARD FLIGHT POWER 359 13.5 L/D OF THE HELICOPTER 3 61 13.6 FORWARD
FLIGHT ANALYSIS 362 13.7 PROPULSIVE EFFICIENCY 366 13.8 CLIMB
PERFORMANCE 367 13.9 PERFORMANCE OF TANDEM HELICOPTERS 370 13.10 SINGLE
OR TANDEM HELICOPTER? 377 PROBLEMS 380 14 ROTORCRAFT MANEUVER 383 14.1
LIMITS ON FLIGHT ENVELOPES 383 14.2 KINETIC ENERGY OF THE ROTOR 385 14.3
AUTOROTATIVE INDEX 387 14.4 AUTOROTATIVE PERFORMANCE 389 14.5
HEIGHT/VELOCITY DIAGRAM 398 14.6 THE VORTEX RING STATE 400 14.7 TAKE-OFF
AND LANDING 404 14.8 TURN PERFORMANCE 404 14.9 POWER REQUIRED FOR
TURNING 406 14.10 MORE ON TAIL ROTOR PERFORMANCE 410 PROBLEMS 412 15
ROTORCRAFT MISSION ANALYSIS 413 15.1 SPECIFIC AIR RANGE 413 15.2
NON-DIMENSIONAL ANALYSIS OF THE SAR 415 15.3 ENDURANCE AND SPECIFIC
ENDURANCE 416 15.4 SPEED FOR MINIMUM POWER 417 15.5 SPEED FOR MAXIMUM
RANGE 419 15.6 FUEL TO CLIMB 420 15.7 PAYLOAD/RANGE DIAGRAM 422 15.8
COMPARATIVE PAYLOAD FRACTION 428 15.9 MISSION ANALYSIS 429 PROBLEMS ^
430 PART III V/STOL AND NOISE PERFORMANCE 16 V/STOL PERFORMANCE 435 16.1
HOVER CHARACTERISTICS 435 16.2. JET-INDUCED LIFT 437 16.3 LIFT
AUGMENTATION 440 16.4 CALCULATION OF SHORT TAKE-OFF 441 16.5 SKI JUMP
445 X CONTENTS 16.6 CONVERTIPLANES OR TILT ROTORS 448 16.7 V/STOL FLIGHT
ENVELOPES 449 PROBLEMS 449 17 NOISE PERFORMANCE 451 17.1 DEFINITIONS OF
SOUND AND NOISE 452 17.2 TRENDS IN NOISE REDUCTION 454 17.3 AIRFRAME
NOISE OF FIXED-WING AIRCRAFT 456 17.4 ENGINE NOISE 460 17.5 NOISE
CERTIFICATION PROCEDURE 461 17.6 NOISE REDUCTION FROM OPERATIONS 464
17.7 MINIMUM NOISE TO CLIMB 467 17.8 HELICOPTER NOISE 469 17.9
HELICOPTER NOISE REDUCTION 472 17.10 NOISE CERTIFICATION OF CIVIL
HELICOPTERS 472 17.11 SONIC BOOM 473 PROBLEMS 478 APPENDIX A AIRCRAFT
MODELS 479 A. 1 AIRCRAFT A: SUBSONIC COMMERCIAL JET 479 A.2 AIRCRAFT B:
TURBOPROP TRANSPORT AIRCRAFT 484 A.3 AIRCRAFT C: SUPERSONIC JET FIGHTER
487 A.4 AIRCRAFT D: GENERAL UTILITY HELICOPTER 494 A.5 AIRCRAFT E:
TANDEM HELICOPTER 502 APPENDIX B NOISE DATA 507 APPENDIX C SELECTED
SIMULATION PROGRAMS 509 C. 1 ASSEMBLING AIRCRAFT FORCES 509 C.2
CALCULATION OF NUMERICAL DERIVATIVES 510 C.3 OPTIMAL CLIMB OF FIGHTER
JET AIRCRAFT 510 C.4 OPTIMAL CLIMB RATE OF TURBOPROP 513 C.5 CALCULATION
OF MISSION FUEL 515 C.6 SUPERSONIC ACCELERATION 518 C.7 ASYMMETRIC
THRUST CONTROL 521 C.8 HOVER POWER WITH BLADE ELEMENT THEORY 524 C.9
FORWARD FLIGHT POWER OF HELICOPTER 526 BIBLIOGRAPHY 531 INDEX 553 |
| any_adam_object | 1 |
| any_adam_object_boolean | 1 |
| author | Filippone, Antonio |
| author_facet | Filippone, Antonio |
| author_role | aut |
| author_sort | Filippone, Antonio |
| author_variant | a f af |
| building | Verbundindex |
| bvnumber | BV021769948 |
| callnumber-first | T - Technology |
| callnumber-label | TL671 |
| callnumber-raw | TL671.4 |
| callnumber-search | TL671.4 |
| callnumber-sort | TL 3671.4 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_rvk | ZO 7250 |
| classification_tum | VER 530f |
| ctrlnum | (OCoLC)255246508 (DE-599)BVBBV021769948 |
| dewey-full | 629.132 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.132 |
| dewey-search | 629.132 |
| dewey-sort | 3629.132 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehrstechnik Verkehr / Transport |
| discipline_str_mv | Verkehrstechnik Verkehr / Transport |
| edition | 1. ed. |
| format | Book |
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| id | DE-604.BV021769948 |
| illustrated | Illustrated |
| index_date | 2024-07-02T15:38:02Z |
| indexdate | 2024-07-09T20:43:40Z |
| institution | BVB |
| isbn | 0750668172 9780750668170 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-014982892 |
| oclc_num | 255246508 |
| open_access_boolean | |
| owner | DE-91G DE-BY-TUM DE-Aug4 DE-634 DE-573 |
| owner_facet | DE-91G DE-BY-TUM DE-Aug4 DE-634 DE-573 |
| physical | XXVII, 565 S. Ill., graph. Darst. |
| publishDate | 2006 |
| publishDateSearch | 2006 |
| publishDateSort | 2006 |
| publisher | Elsevier |
| record_format | marc |
| series2 | Elsevier aerospace engineering series |
| spelling | Filippone, Antonio Verfasser aut Flight performance of fixed and rotary wing aircraft Antonio Filippone 1. ed. Amsterdam [u.a.] Elsevier 2006 XXVII, 565 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Elsevier aerospace engineering series Aerospace engineering Airplanes Performance Flight engineering 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=014982892&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Filippone, Antonio Flight performance of fixed and rotary wing aircraft Aerospace engineering Airplanes Performance Flight engineering Flugmechanik (DE-588)4154760-3 gnd |
| subject_GND | (DE-588)4154760-3 |
| title | Flight performance of fixed and rotary wing aircraft |
| title_auth | Flight performance of fixed and rotary wing aircraft |
| title_exact_search | Flight performance of fixed and rotary wing aircraft |
| title_exact_search_txtP | Flight performance of fixed and rotary wing aircraft |
| title_full | Flight performance of fixed and rotary wing aircraft Antonio Filippone |
| title_fullStr | Flight performance of fixed and rotary wing aircraft Antonio Filippone |
| title_full_unstemmed | Flight performance of fixed and rotary wing aircraft Antonio Filippone |
| title_short | Flight performance of fixed and rotary wing aircraft |
| title_sort | flight performance of fixed and rotary wing aircraft |
| topic | Aerospace engineering Airplanes Performance Flight engineering Flugmechanik (DE-588)4154760-3 gnd |
| topic_facet | Aerospace engineering Airplanes Performance Flight engineering Flugmechanik |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=014982892&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT filipponeantonio flightperformanceoffixedandrotarywingaircraft |