Aircraft design: a systems engineering approach
"Presenting in one volume the methodologies behind aircraft design, this book uses a systems engineering approach to cover the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics and controls, are covered first of all...
Gespeichert in:
| Beteilige Person: | |
|---|---|
| Format: | Buch |
| Sprache: | Englisch |
| Veröffentlicht: |
Hoboken, New Jersey
Wiley
2013
|
| Schriftenreihe: | Aerospace series
|
| Schlagwörter: | |
| Links: | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=025386791&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| Zusammenfassung: | "Presenting in one volume the methodologies behind aircraft design, this book uses a systems engineering approach to cover the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics and controls, are covered first of all. The author then explains the design process in a holistic manner to emphasize the integration of individual components into the overall design. Throughout the book, the various design options are considered and weighed against each other, to give readers a practical understanding of the process overall"-- Provided by publisher. -- "Presenting in one volume the methodologies behind aircraft design, this book uses a systems engineering approach to cover the components and the issues affected by design procedures"-- Provided by publisher. |
| Beschreibung: | Literaturangaben Includes bibliographical references and index |
| Umfang: | XXX, 778 S. Ill., graph. Darst. 25 cm |
| ISBN: | 9781119953401 |
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| 245 | 1 | 0 | |a Aircraft design |b a systems engineering approach |c Mohammad H. Sadraey |
| 264 | 1 | |a Hoboken, New Jersey |b Wiley |c 2013 | |
| 300 | |a XXX, 778 S. |b Ill., graph. Darst. |c 25 cm | ||
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| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 0 | |a Aerospace series | |
| 500 | |a Literaturangaben | ||
| 500 | |a Includes bibliographical references and index | ||
| 520 | |a "Presenting in one volume the methodologies behind aircraft design, this book uses a systems engineering approach to cover the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics and controls, are covered first of all. The author then explains the design process in a holistic manner to emphasize the integration of individual components into the overall design. Throughout the book, the various design options are considered and weighed against each other, to give readers a practical understanding of the process overall"-- Provided by publisher. -- "Presenting in one volume the methodologies behind aircraft design, this book uses a systems engineering approach to cover the components and the issues affected by design procedures"-- Provided by publisher. | ||
| 650 | 4 | |a Airplanes |x Design and construction | |
| 650 | 7 | |a TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics |2 bisacsh | |
| 650 | 0 | 7 | |a Konstruktion |0 (DE-588)4032231-2 |2 gnd |9 rswk-swf |
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| 943 | 1 | |a oai:aleph.bib-bvb.de:BVB01-025386791 | |
Datensatz im Suchindex
| _version_ | 1819368515909451776 |
|---|---|
| adam_text | IMAGE 1
CONTENTS
PREFACE
SERIES PREFACE
ACKNOWLEDGMENTS
SYMBOLS AND ACRONYMS
1 AIRCRAFT DESIGN FUNDAMENTALS 1.1 INTRODUCTION TO DESIGN 1.2
ENGINEERING DESIGN 1.3 DESIGN PROJECT PLANNING
1.4 DECISION MAKING 1.5 FEASIBILITY ANALYSIS 1.6 TORT OF NEGLIGENCE
REFERENCES
2
2.1 2.2 2.3
SYSTEMS ENGINEERING APPROACH INTRODUCTION FUNDAMENTALS OF SYSTEMS
ENGINEERING CONCEPTUAL SYSTEM DESIGN
2.3.1 DEFINITION
2.3.2 CONCEPTUAL DESIGN FLOWCHART 2.3.3 TECHNICAL PERFORMANCE MEASURES
2.3.4 FUNCTIONAL ANALYSIS 2: 3.5 SYSTEM TRADE-OFF ANALYSIS
2.3.6 CONCEPTUAL DESIGN REVIEW 2.4 PRELIMINARY SYSTEM DESIGN 2.5 DETAIL
SYSTEM DESIGN 2.6 DESIGN REQUIREMENTS
2.7 DESIGN REVIEW, EVALUATION, AND FEEDBACK 2.8 SYSTEMS ENGINEERING
APPROACH IN AIRCRAFT DESIGN 2.8.1 IMPLEMENTATION OF SYSTEMS ENGINEERING
XV
XIX
XXI
XXIII
1
4
8
10 12 15
17
19 19 20 23
23 24 25 26
27 28 29 30
33 34 37 37
IMAGE 2
VIII
2.8.2 DESIGN PHASES 2.8.3 DESIGN FLOWCHART 2.8.4 DESIGN GROUPS 2.8.5
DESIGN STEPS
REFERENCES
3 AIRCRAFT CONCEPTUAL DESIGN
3.1 INTRODUCTION 3.2 PRIMARY FUNCTIONS OF AIRCRAFT COMPONENTS 3.3
AIRCRAFT CONFIGURATION ALTERNATIVES 3.3.1 WING CONFIGURATION
3.3.2 TAIL CONFIGURATION 3.3.3 PROPULSION SYSTEM CONFIGURATION 3.3.4
LANDING GEAR CONFIGURATION 3.3.5 FUSELAGE CONFIGURATION
3.3.6 MANUFACTURING-RELATED ITEMS CONFIGURATION 3.3.7 SUBSYSTEMS
CONFIGURATION 3.4 AIRCRAFT CLASSIFICATION AND DESIGN CONSTRAINTS 3.5
CONFIGURATION SELECTION PROCESS AND TRADE-OFF ANALYSIS
3.6 CONCEPTUAL DESIGN OPTIMIZATION 3.6.1 MATHEMATICAL TOOLS 3.6.2
METHODOLOGY PROBLEMS REFERENCES
4
4.1 4.2
4.2.2 4.2.3 4.2.4 4.2.5 4.2.6 4.2.7
PRELIMINARY DESIGN INTRODUCTION MAXIMUM TAKE-OFF WEIGHT ESTIMATION 4.2.1
THE GENERAL TECHNIQUE
WEIGHT BUILD-UP PAYLOAD WEIGHT CREW WEIGHT FUEL WEIGHT EMPTY WEIGHT
PRACTICAL STEPS OF THE TECHNIQUE
4.3 WING AREA AND ENGINE SIZING 4.3.1 SUMMARY OF THE TECHNIQUE 4.3.2
STALL SPEED
4.3.3 MAXIMUM SPEED 4.3.4 TAKE-OFF RUN 4.3.5 RATE OF CLIMB
4.3.6 CEILING
4.4 DESIGN EXAMPLES PROBLEMS REFERENCES
CONTENTS
38 39 41 43
47
49 49 50 52
53 55 55
56 58 58
59 62 68
74 74 76 86 92
93 93 94
94 95 96 97 100
108 112 113 113
118 120 131 136
140 145 155 158
IMAGE 3
CONTENTS
5 WING DESIGN
5.1 INTRODUCTION 5.2 NUMBER OF WINGS 5.3 WING VERTICAL LOCATION 5.3.1
HIGH WING
5.3.2 LOW WING
5.3.3 MID-WING
5.3.4 PARASOL WING
5.3.5 THE SELECTION PROCESS 5.4 AIRFOIL SECTION
5.4.1 AIRFOIL DESIGN OR AIRFOIL SELECTION 5.4.2 GENERAL FEATURES OF AN
AIRFOIL 5.4.3 CHARACTERISTIC GRAPHS OF AN AIRFOIL 5.4.4 AIRFOIL
SELECTION CRITERIA 5.4.5 NACA AIRFOILS 5.4.6 PRACTICAL STEPS FOR WING
AIRFOIL SECTION SELECTION 5.5 WING INCIDENCE 5.6 ASPECT RATIO
5.7 TAPER RATIO
5.8 THE SIGNIFICANCE OF LIFT AND LOAD DISTRIBUTIONS 5.9 SWEEP ANGLE 5.10
TWIST ANGLE 5.11 DIHEDRAL ANGLE 5.12 HIGH-LIFT DEVICE
5.12.1 THE FUNCTIONS OF A HIGH-LIFT DEVICE 5.12.2 HIGH-LIFT DEVICE
CLASSIFICATION 5.12.3 DESIGN TECHNIQUE 5.13 AILERON 5.14 LIFTING-LINE
THEORY 5.15 ACCESSORIES
5.15.1 STRAKE 5.15.2 FENCE 5.15.3 VORTEX GENERATOR 5.15.4 WINGLET 5.16
WING DESIGN STEPS 5.17 WING DESIGN EXAMPLE
PROBLEMS REFERENCES
6 TAIL DESIGN
6.1 INTRODUCTION 6.2 AIRCRAFT TRIM REQUIREMENTS 6.2.1 LONGITUDINAL TRIM
6.2.2 DIRECTIONAL AND LATERAL TRIM
6.3 A REVIEW ON STABILITY AND CONTROL
IX
161 161 164 165
165 168 169
169 169 170
171 173 176 182 183 188 195 198 203 206 209 223 226 230 230 232 235 241
242 246
247 247 248 248 249 250 259 264
265 265 268 270
276 278
IMAGE 4
X CONTENTS
6.3.1 STABILITY
6.3.2 CONTROL
6.3.3 HANDLING QUALITIES 6.4 TAIL CONFIGURATION 6.4.1 BASIC TAIL
CONFIGURATION 6.4.2 AFT TAIL CONFIGURATION
6.5 CANARD OR AFT TAIL
6.6 OPTIMUM TAIL ARM
6.7 HORIZONTAL TAIL PARAMETERS 6.7.1 HORIZONTAL TAIL DESIGN FUNDAMENTAL
GOVERNING EQUATION 6.7.2 FIXED, ALL-MOVING, OR ADJUSTABLE 6.7.3 AIRFOIL
SECTION
6.7.4 TAIL INCIDENCE 6.7.5 ASPECT RATIO 6.7.6 TAPER RATIO
6.7.7 SWEEP ANGLE 6.7.8 DIHEDRAL ANGLE
6.7.9 TAIL VERTICAL LOCATION 6.7.10 OTHER TAIL GEOMETRIES 6.7.11 CONTROL
PROVISION 6.7.12 FINAL CHECK 6.8 VERTICAL TAIL DESIGN
6.8.1 VERTICAL TAIL DESIGN REQUIREMENTS 6.8.2 VERTICAL TAIL PARAMETERS
6.9 PRACTICAL DESIGN STEPS 6.10 TAIL DESIGN EXAMPLE
PROBLEMS REFERENCES
7 FUSELAGE DESIGN
7.1 INTRODUCTION 7.2 FUNCTIONAL ANALYSIS AND DESIGN FLOWCHART 7.3
FUSELAGE CONFIGURATION DESIGN AND INTERNAL ARRANGEMENT 7.4 ERGONOMICS
7.4.1 DEFINITIONS 7.4.2 HUMAN DIMENSIONS AND LIMITS 7.5 COCKPIT DESIGN
7.5.1 NUMBER OF PILOTS AND CREW MEMBERS
7.5.2 PILOT/CREW MISSION 7.5.3 PILOT/CREW COMFORT/HARDSHIP LEVEL 7.5.4
PILOT PERSONAL EQUIPMENT 7.5.5 CONTROL EQUIPMENT
7.5.6 MEASUREMENT EQUIPMENT 7.5.7 LEVEL OF AUTOMATION 7.5.8 EXTERNAL
CONSTRAINTS
278 282 284 285 285 288 294 298 301
301 304 306 308
311 312 313 313
314 315 316 316 317
317 319 329 331 336 340
341 341 341 345 346
346 348 350 351
353 353 354 355 356 357 359
IMAGE 5
CONTENTS XI
7.5.9 COCKPIT INTEGRATION 359
7.6 PASSENGER CABIN DESIGN 360
7.7 CARGO SECTION DESIGN 368
7.8 OPTIMUM LENGTH-TO-DIAMETER RATIO 372
7.8.1 OPTIMUM SLENDERNESS RATIO FOR LOWEST7LD 372
7.8.2 OPTIMUM SLENDERNESS RATIO FOR LOWEST FUSELAGE WETTED AREA 378
7.8.3 OPTIMUM SLENDERNESS RATIO FOR THE LIGHTEST FUSELAGE 380
7.9 OTHER FUSELAGE INTERNAL SEGMENTS 380
7.9.1 FUEL TANKS 381
7.9.2 RADAR DISH 385
7.9.3 WING BOX 386
7.9.4 POWER TRANSMISSION SYSTEMS 387
7.10 LOFTING 388
7.10.1 AERODYNAMICS CONSIDERATIONS 388
7.10.2 AREA RULING 390
7.10.3 RADAR DETECTABILITY 392
7.10.4 FUSELAGE REAR SECTION 392
7.11 FUSELAGE DESIGN STEPS 394
7.12 DESIGN EXAMPLE 395
PROBLEMS 406
REFERENCES 410
8 PROPULSION SYSTEM DESIGN 413
8.1 INTRODUCTION 413
8.2 FUNCTIONAL ANALYSIS AND DESIGN REQUIREMENTS 414
8.3 ENGINE TYPE SELECTION 416
8.3.1 AIRCRAFT ENGINE CLASSIFICATION 417
8.3.2 SELECTION OF ENGINE TYPE 428
8.4 NUMBER OF ENGINES 436
8.4.1 FLIGHT SAFETY 437
8.4.2 OTHER INFLUENTIAL PARAMETERS 438
8.5 ENGINE LOCATION 439
8.5.1 DESIGN REQUIREMENTS 439
8.5.2 GENERAL GUIDELINES 441
8.5.3 PODDED VERSUS BURIED 443
8.5.4 PUSHER VERSUS TRACTOR 444
8.5.5 TWIN-JET ENGINE: UNDER-WING VERSUS REAR FUSELAGE 446
8.6 ENGINE INSTALLATION 448
8.6.1 PROP-DRIVEN ENGINE 450
8.6.2 JET ENGINE 452
8.7 PROPELLER SIZING 456
8.8 ENGINE PERFORMANCE 461
8.8.1 PROP-DRIVEN ENGINE 461
8.8.2 JET ENGINE 462
8.9 ENGINE SELECTION 462
IMAGE 6
XII CONTENTS
8.10 PROPULSION SYSTEM DESIGN STEPS 8.11 DESIGN EXAMPLE PROBLEMS
REFERENCES
9 LANDING GEAR DESIGN
9.1 INTRODUCTION 9.2 FUNCTIONAL ANALYSIS AND DESIGN REQUIREMENTS 9.3
LANDING GEAR CONFIGURATION 9.3.1 SINGLE MAIN
9.3.2 BICYCLE
9.3.3 TAIL-GEAR
9.3.4 TRICYCLE
9.3.5 QUADRICYCLE 9.3.6 MULTI-BOGEY 9.3.7 RELEASABLE RAIL 9.3.8 SKID
9.3.9 SEAPLANE LANDING DEVICE 9.3.10 HUMAN LEG 9.3.11 LANDING GEAR
CONFIGURATION SELECTION PROCESS 9.3.12 LANDING GEAR ATTACHMENT 9.4
FIXED, RETRACTABLE, OR SEPARABLE LANDING GEAR
9.5 LANDING GEAR GEOMETRY 9.5.1 LANDING GEAR HEIGHT 9.5.2 WHEEL BASE
9.5.3 WHEEL TRACK
9.6 LANDING GEAR AND AIRCRAFT CENTER OF GRAVITY 9.6.1 TIPBACK AND
TIPFORWARD ANGLE REQUIREMENTS 9.6.2 TAKE-OFF ROTATION REQUIREMENT 9.7
LANDING GEAR MECHANICAL SUBSYSTEMS/PARAMETERS
9.7.1 TIRE SIZING
9.7.2 SHOCK ABSORBER 9.7.3 STRUT SIZING
9.7.4 STEERING SUBSYSTEM 9.7.5 LANDING GEAR RETRACTION SYSTEM 9.8
LANDING GEAR DESIGN STEPS 9.9 LANDING GEAR DESIGN EXAMPLE
PROBLEMS REFERENCES
10 WEIGHT OF COMPONENTS 10.1 INTRODUCTION 10.2 SENSITIVITY OF WEIGHT
CALCULATION 10.3 AIRCRAFT MAJOR COMPONENTS
10.4 WEIGHT CALCULATION TECHNIQUE 10.4.1 WING WEIGHT
464 467 471 478
479 479 481 484
484 485 487 487
488 489 489 489 490
491 492 493 494 497
498 503 508
516 516 518 524
524 525 526 527
527 528 529
539 544
547 547 549 553
556 559
IMAGE 7
CONTENTS
10.5
10.4.2 10.4.3 10.4.4 10.4.5 10.4.6 10.4.7
10.4.8
HORIZONTAL TAIL WEIGHT VERTICAL TAIL WEIGHT FUSELAGE WEIGHT LANDING GEAR
WEIGHT INSTALLED ENGINE WEIGHT
FUEL SYSTEM WEIGHT WEIGHT OF OTHER EQUIPMENT AND SUBSYSTEMS CHAPTER
EXAMPLES PROBLEMS REFERENCES
11 AIRCRAFT WEIGHT DISTRIBUTION 11.1 INTRODUCTION 11.2 AIRCRAFT CENTER
OF GRAVITY CALCULATION 11.3 CENTER OF GRAVITY RANGE
11.3.1 FIXED OR VARIABLE CENTER OF GRAVITY 11.3.2 CENTER OF GRAVITY
RANGE DEFINITION 11.3.3 IDEAL CENTER OF GRAVITY LOCATION
X111
561 561 562 563
564 564 565 565 570 573
575 575 578 585
585 586 587
1 1.4 LONGITUDINAL CENTER OF GRAVITY LOCATION 590
11.5 TECHNIQUE TO DETERMINE THE AIRCRAFT FORWARD AND AFT CENTER OF
GRAVITY 598 11.6 WEIGHT DISTRIBUTION TECHNIQUE 606
11.6.1 FUNDAMENTALS OF WEIGHT DISTRIBUTION 607
11.6.2 LONGITUDINAL STABILITY REQUIREMENTS 609
11.6.3 LONGITUDINAL CONTROLLABILITY REQUIREMENTS 611
11.6.4 LONGITUDINAL HANDLING QUALITY REQUIREMENTS 613
11.7 AIRCRAFT MASS MOMENT OF INERTIA 11.8 CHAPTER EXAMPLE PROBLEMS
REFERENCES
615 620 624 630
12 DESIGN OF CONTROL SURFACES 631
12.1 INTRODUCTION 631
12.2 CONFIGURATION SELECTION OF CONTROL SURFACES 637
12.3 HANDLING QUALITIES 638
12.3.1 DEFINITIONS 640
12.3.2 LONGITUDINAL HANDLING QUALITIES 643
12.3.3 LATERAL-DIRECTIONAL HANDLING QUALITIES 647
12.4 AILERON DESIGN 654
12.4.1 INTRODUCTION 654
12.4.2 PRINCIPLES OF AILERON DESIGN 656
12.4.3 AILERON DESIGN CONSTRAINTS 664
12.4.4 STEPS IN AILERON DESIGN 669
12.5 ELEVATOR DESIGN 670
12.5.1 INTRODUCTION 670
12.5.2 PRINCIPLES OF ELEVATOR DESIGN 672
12.5.3 TAKE-OFF ROTATION REQUIREMENT 676
IMAGE 8
XIV
12.5.4 LONGITUDINAL TRIM REQUIREMENT 12.5.5 ELEVATOR DESIGN PROCEDURE
12.6 RUDDER DESIGN 12.6.1 INTRODUCTION TO RUDDER DESIGN
12.6.2 FUNDAMENTALS OF RUDDER DESIGN 12.6.3 RUDDER DESIGN STEPS 12.7
AERODYNAMIC BALANCE AND MASS BALANCE 12.7.1 AERODYNAMIC BALANCE
12.7.2 MASS BALANCE 12.8 CHAPTER EXAMPLES 12.8.1 AILERON DESIGN EXAMPLE
12.8.2 ELEVATOR DESIGN EXAMPLE
12.8.3 RUDDER DESIGN EXAMPLE PROBLEMS REFERENCES
APPENDICES APPENDIX A: STANDARD ATMOSPHERE, SI UNITS APPENDIX B:
STANDARD ATMOSPHERE, BRITISH UNITS
CONTENTS
680 683 685 685
688 709 713 715
722 723 723 729
738 745 752
755 755 756
INDEX 757
|
| any_adam_object | 1 |
| author | Sadraey, Mohammad H. |
| author_GND | (DE-588)1027749941 |
| author_facet | Sadraey, Mohammad H. |
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| author_sort | Sadraey, Mohammad H. |
| author_variant | m h s mh mhs |
| building | Verbundindex |
| bvnumber | BV040540885 |
| callnumber-first | T - Technology |
| callnumber-label | TL671 |
| callnumber-raw | TL671.2 |
| callnumber-search | TL671.2 |
| callnumber-sort | TL 3671.2 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_rvk | ZO 7200 |
| ctrlnum | (OCoLC)820395285 (DE-599)BVBBV040540885 |
| dewey-full | 629.134/1 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.134/1 |
| dewey-search | 629.134/1 |
| dewey-sort | 3629.134 11 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| format | Book |
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| id | DE-604.BV040540885 |
| illustrated | Illustrated |
| indexdate | 2024-12-20T16:17:18Z |
| institution | BVB |
| isbn | 9781119953401 |
| language | English |
| lccn | 2012009907 |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-025386791 |
| oclc_num | 820395285 |
| open_access_boolean | |
| owner | DE-M347 DE-573 DE-210 DE-706 |
| owner_facet | DE-M347 DE-573 DE-210 DE-706 |
| physical | XXX, 778 S. Ill., graph. Darst. 25 cm |
| publishDate | 2013 |
| publishDateSearch | 2013 |
| publishDateSort | 2013 |
| publisher | Wiley |
| record_format | marc |
| series2 | Aerospace series |
| spellingShingle | Sadraey, Mohammad H. Aircraft design a systems engineering approach Airplanes Design and construction TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics bisacsh Konstruktion (DE-588)4032231-2 gnd Flugzeugbau (DE-588)4154782-2 gnd Entwurf (DE-588)4121208-3 gnd |
| subject_GND | (DE-588)4032231-2 (DE-588)4154782-2 (DE-588)4121208-3 |
| title | Aircraft design a systems engineering approach |
| title_auth | Aircraft design a systems engineering approach |
| title_exact_search | Aircraft design a systems engineering approach |
| title_full | Aircraft design a systems engineering approach Mohammad H. Sadraey |
| title_fullStr | Aircraft design a systems engineering approach Mohammad H. Sadraey |
| title_full_unstemmed | Aircraft design a systems engineering approach Mohammad H. Sadraey |
| title_short | Aircraft design |
| title_sort | aircraft design a systems engineering approach |
| title_sub | a systems engineering approach |
| topic | Airplanes Design and construction TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics bisacsh Konstruktion (DE-588)4032231-2 gnd Flugzeugbau (DE-588)4154782-2 gnd Entwurf (DE-588)4121208-3 gnd |
| topic_facet | Airplanes Design and construction TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics Konstruktion Flugzeugbau Entwurf |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=025386791&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT sadraeymohammadh aircraftdesignasystemsengineeringapproach |