Aircraft performance and design:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Boston
McGraw-Hill
1999
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XVI, 580 S. graph. Darst. |
| ISBN: | 0070019711 0071160108 |
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Datensatz im Suchindex
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| adam_text | AIRCRAFT PERFORMANCE AND DESIGN JOHN D. ANDERSON, JR. UNIVERSITY OF
MARYLAND WCB MCGRAW-HILL BOSTON BURR RIDGE, IL DUBUQUE, IA MADISON, WI
NEW YORK SAN FRANCISCO ST. LOUIS BANGKOK BOGOTA CARACAS LISBON LONDON
MADRID MEXICO CITY MILAN NEW DELHI SEOUL SINGAPORE SYDNEY TAIPEI TORONTO
CONTENTS PREFACE IX PART 1 PRELIMINARY CONSIDERATIONS 1 CHAPTER 1 THE
EVOLUTION OF THE AIRPLANE AND ITS PERFORMANCE: A SHORT HISTORY 3 1.1
INTRODUCTION 3 1.2 FOUR HISTORICAL PERIODS OF AIRPLANE DESIGN
CHARACTERISTICS 6 1.2.1 PRE-WRIGHT ERA 6 1.2.2 ERA OF STRUT-AND-WIRE
BIPLANES 15 1.2.3 ERA OF THE MATURE, PROPELLER-DRIVEN AIRPLANE 23 1.2.4
ERA OF THE JET-PROPELLED AIRPLANE 33 1.3 UNCONVENTIONAL DESIGNS
(INNOVATIVE CONCEPTS) 43 1.4 SUMMARY AND THE FUTURE 47 CHAPTER 2
AERODYNAMICS OF THE AIRPLANE: THE DRAG POLAR 51 2.1 INTRODUCTION 51 2.2
THE SOURCE OF AERODYNAMIC FORCE 52 2.3 AERODYNAMIC LIFT, DRAG, AND
MOMENTS 53 2.4 AERODYNAMIC COEFFICIENTS 57 2.5 LIFT, DRAG, AND MOMENT
COEFFICIENTS: HOW THEY VARY 62 2.6 THE AERODYNAMIC CENTER 70 2.7 NACA
AIRFOIL NOMENCLATURE 73 2.8 LIFT AND DRAG BUILDUP 78 2.8.1 LIFT FOR A
FINITE WING 78 2.8.2 WING-BODY COMBINATIONS 103 2.8.3 DRAG 105 2.8.4
SUMMARY 124 2.9 THE DRAG POLAR 126 2.9.1 MORE THOUGHTS ON DRAG 126 2.9.2
THE DRAG POLAR: WHAT IS IT AND HOW IS IT USED? 129 2.10 HISTORICAL NOTE:
THE ORIGIN OF THE DRAG POLAR*LILIENTHAL AND EIFFEL 137 2.11 SUMMARY 141
CHAPTER 3 SOME PROPULSION CHARACTERISTICS 145 3.1 INTRODUCTION 145 3.2
THRUST AND EFFICIENCY*THE TRADEOFF 146 3.3 THE RECIPROCATING
ENGINE/PROPELLER COMBINATION 151 3.3.1 VARIATIONS OF POWER AND SPECIFIC
FUEL CONSUMPTION WITH VELOCITY AND ALTITUDE 154 3.3.2 THE PROPELLER 156
3.4 THE TURBOJET ENGINE 162 3.4.1 VARIATIONS OF THRUST AND SPECIFIC FUEL
CONSUMPTION WITH VELOCITY AND ALTITUDE 166 3.5 THE TURBOFAN ENGINE 170
3.5.1 VARIATIONS OF THRUST AND SPECIFIC FUEL CONSUMPTION WITH VELOCITY
AND ALTITUDE 174 3.6 THE TURBOPROP 178 3.6.1 VARIATIONS OF POWER AND
SPECIFIC FUEL CONSUMPTION WITH VELOCITY AND ALTITUDE 181 3.7
MISCELLANEOUS COMMENTS: AFTERBURNING AND MORE ON SPECIFIC FUEL
CONSUMPTION 183 3.8 SUMMARY 185 CONTENTS PART 2 AIRPLANE PERFORMANCE 189
CHAPTER 4 THE EQUATIONS OF MOTION 191 4.1 INTRODUCTION 191 4.2 THE FOUR
FORCES OF FLIGHT 192 4.3 THE EQUATIONS OF MOTION 194 4.4 SUMMARY AND
COMMENTS 197 CHAPTER 5 AIRPLANE PERFORMANCE: STEADY FLIGHT 199 5.1
INTRODUCTION 199 5.2 EQUATIONS OF MOTION FOR STEADY, LEVEL FLIGHT 201
5.3 THRUST REQUIRED (DRAG) 202 5.3.1 GRAPHICAL APPROACH 202 5.3.2
ANALYTICAL APPROACH 208 5.3.3 GRAPHICAL AND ANALYTICAL APPROACHES: SOME
COMMENTS 216 5.4 THE FUNDAMENTAL PARAMETERS: THRUST-TO-WEIGHT RATIO,
WING LOADING, DRAG POLAR, AND LIFT-TO-DRAG RATIO 216 5.4.1 AERODYNAMIC
RELATIONS ASSOCIATED WITH MAXIMUM C L /C D , C 3L/2 /C D , AND C[ /2 /C
D 218 5.5 THRUST AVAILABLE AND THE MAXIMUM VELOCITY OF THE AIRPLANE 226
5.5.1 PROPELLER-DRIVEN AIRCRAFT 227 5.5.2 JET-PROPELLED AIRCRAFT 229
5.5.3 MAXIMUM VELOCITY 230 5.6 POWER REQUIRED 234 5.6.1 GRAPHICAL
APPROACH 235 5.6.2 ANALYTICAL APPROACH 236 5.7 POWER AVAILABLE AND
MAXIMUM VELOCITY 239 5.7.1 PROPELLER-DRIVEN AIRCRAFT 239 5.7.2 TURBOJET
AND TURBOFAN ENGINES 241 5.7.3 MAXIMUM VELOCITY 242 5.8 EFFECT OF DRAG
DIVERGENCE ON MAXIMUM VELOCITY 244 5.9 MINIMUM VELOCITY: STALL AND
HIGH-LIFT DEVICES 252 5.10 5.11 5.12 5.13 5.14 5.15 5.16 5.9.1 5.9.2
5.9.3 5.9.4 CALCULATION OF STALLING VELOCITY: ROLE OF(CJ MAX 253 THE
NATURE OF STALL*FLOW SEPARATION 255 HIGH-LIFT DEVICES 257 INTERIM
SUMMARY 263 RATE OF CLIMB 265 5.10.1 5.10.2 5.10.3 SERVICE TIME TO
5.12.1 5.12.2 RANGE 5.13.1 5.13.2 5.13.3 GRAPHICAL APPROACH 268
ANALYTICAL APPROACH 270 GLIDING (UNPOWERED) FLIGHT 282 AND ABSOLUTE
CEILINGS 287 CLIMB 290 GRAPHICAL APPROACH 290 ANALYTICAL APPROACH 292
293 RANGE FOR PROPELLER-DRIVEN AIRPLANES 296 RANGE FOR JET-PROPELLED
AIRPLANES 297 OTHER CONSIDERATIONS 299 ENDURANCE 302 5.14.1 5.14.2
ENDURANCE FOR PROPELLER-DRIVEN AIRPLANES 303 ENDURANCE FOR JET-PROPELLED
AIRPLANES 305 RANGE AND ENDURANCE: A SUMMARY AND SOME GENERAL THOUGHTS
305 5.15.1 5.15.2 5.15.3 5.15.4 MORE ON ENDURANCE 306 MORE ON RANGE 308
GRAPHICAL SUMMARY 309 THE EFFECT OF WIND 309 SUMMARY 314 CHAPTER 6
AIRPLANE PERFORMANCE: ACCELERATED FLIGHT 321 6.1 INTRODUCTION 321 6.2
LEVEL TURN 322 6.2.1 MINIMUM TURN RADIUS 329 6.2.2 MAXIMUM TURN RATE 332
6.3 THE PULL-UP AND PULLDOWN MANEUVERS 336 6.4 LIMITING CASE FOR LARGE
LOAD FACTOR 339 6.5 THE V-N DIAGRAM 341 CONTENTS 6.6 ENERGY CONCEPTS:
ACCELERATED RATE OF CLIMB 344 6.7 TAKEOFF PERFORMANCE 353 6.7.1
CALCULATION OF GROUND ROLL 355 6.7.2 CALCULATION OF DISTANCE WHILE
AIRBORNE TO CLEAR AN OBSTACLE 363 6.8 LANDING PERFORMANCE 367 6.8.1
CALCULATION OF APPROACH DISTANCE 368 6.8.2 CALCULATION OF FLARE DISTANCE
370 6.8.3 CALCULATION OF GROUND ROLL 370 6.9 SUMMARY 375 PART 3 AIRPLANE
DESIGN 379 CHAPTER 7 THE PHILOSOPHY OF AIRPLANE DESIGN 381 7.1 7.2 7.3
INTRODUCTION 381 PHASES OF AIRPLANE DESIGN 382 7.2.1 CONCEPTUAL DESIGN
382 7.2.2 PRELIMINARY DESIGN 383 7.2.3 DETAIL DESIGN 386 7.2.4 INTERIM
SUMMARY 386 THE SEVEN INTELLECTUAL PIVOT POINTS FOR CONCEPTUAL DESIGN
387 7.3.1 7.3.2 7.3.3 7.3.4 7.3.5 7.3.6 7.3.7 7.3.8 7.3.9 REQUIREMENTS
388 WEIGHT OF THE AIRPLANE*FIRST ESTIMATE 389 CRITICAL PERFORMANCE
PARAMETERS CONFIGURATION LAYOUT 391 BETTER WEIGHT ESTIMATE 391
PERFORMANCE ANALYSIS 391 OPTIMIZATION 392 CONSTRAINT DIAGRAM 392 INTERIM
SUMMARY 395 391 CHAPTER 8 DESIGN OF A PROPELLER-DRIVEN AIRPLANE 397 8.1
INTRODUCTION 397 8.2 REQUIREMENTS 398 8.3 THE WEIGHT OF AN AIRPLANE AND
ITS FIRST ESTIMATE 398 8.3.1 ESTIMATION OF WJ W O 399 8.3.2 ESTIMATION
OF W//WO 400 8.3.3 CALCULATION OF W O 405 8.4 ESTIMATION OF THE CRITICAL
PERFORMANCE PARAMETERS 406 8.4.1 MAXIMUM LIFT COEFFICIENT 406 8.4.2 WING
LOADING W/S 410 8.4.3 THRUST-TO-WEIGHT RATIO 412 8.5 SUMMARY OF THE
CRITICAL PERFORMANCE PARAMETERS 419 8.6 CONFIGURATION LAYOUT 419 8.6.1
8.6.2 8.6.3 8.6.4 8.6.5 8.6.6 8.6.7 8.6.8 OVERALL TYPE OF CONFIGURATION
420 WING CONFIGURATION 420 FUSELAGE CONFIGURATION 431 CENTER-OF-GRAVITY
LOCATION: FIRST ESTIMATE 433 HORIZONTAL AND VERTICAL TAIL SIZE 435
PROPELLER SIZE 440 LANDING GEAR, AND WING PLACEMENT 442 THE RESULTING
LAYOUT 448 8.7 A BETTER WEIGHT ESTIMATE 449 8.8 PERFORMANCE ANALYSIS 453
8.8.1 8.8.2 8.8.3 8.8.4 8.8.5 8.8.6 8.8.7 POWER REQUIRED AND POWER
AVAILABLE CURVES 453 RATE OF CLIMB 455 RANGE 455 STALLING SPEED 456
LANDING DISTANCE 456 TAKEOFF DISTANCE 457 INTERIM SUMMARY 458 8.9
SUMMARY 458 8.10 DESIGN CASE STUDY: THE WRIGHT FLYER 458 8.11 DESIGN
CASE STUDY: THE DOUGLAS DC-3 463 CHAPTER 9 DESIGN OF JET-PROPELLED
AIRPLANES 487 9.1 INTRODUCTION 488 9.2 THE DESIGN OF SUBSONIC/TRANSONIC
JET-PROPELLED AIRPLANES: A CASE STUDY OF THE BOEING 707 AND 727 489
CONTENTS 9.2.1 DESIGN OF THE B-47*A PRECURSOR TO THE 707 489 9.2.2
DESIGN OF THE 707 CIVIL JET TRANSPORT 494 9.2.3 DESIGN OF THE BOEING 727
JET TRANSPORT 500 9.2.4 INTERIM SUMMARY 513 9.3 SUBSONIC JET AIRPLANE
DESIGN: ADDITIONAL CONSIDERATIONS 516 9.4 SUPERSONIC AIRPLANE DESIGN 519
9.4.1 DESIGN OF THE F-16 519 9.4.2 DESIGN OF THE SR-71 BLACKBIRD 527
9.4.3 DESIGN OF THE LOCKHEED F-22 ADVANCED TACTICAL FIGHTER 538 9.5
SUMMARY 542 POSTFACE 543 APPENDIX A STANDARD ATMOSPHERE, SI UNITS 545
APPENDIX B STANDARD ATMOSPHERE, ENGLISH ENGINEERING UNITS 557 ANSWERS TO
SELECTED PROBLEMS 567 REFERENCES 569 INDEX 573
|
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| spellingShingle | Anderson, John David 1937- Aircraft performance and design Projetos de aeronaves larpcal Airplanes Design and construction Airplanes Performance Flugzeug (DE-588)4017672-1 gnd Flugleistung (DE-588)4129359-9 gnd Konstruktion (DE-588)4032231-2 gnd |
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| title | Aircraft performance and design |
| title_auth | Aircraft performance and design |
| title_exact_search | Aircraft performance and design |
| title_full | Aircraft performance and design John D. Anderson |
| title_fullStr | Aircraft performance and design John D. Anderson |
| title_full_unstemmed | Aircraft performance and design John D. Anderson |
| title_short | Aircraft performance and design |
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| topic_facet | Projetos de aeronaves Airplanes Design and construction Airplanes Performance Flugzeug Flugleistung Konstruktion |
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