Advanced aircraft design: conceptual design, analysis and optimization of subsonic civil airplanes
Gespeichert in:
| 1. Verfasser: | |
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| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Chichester
Wiley
2013
|
| Schriftenreihe: | Aerospace Series
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| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XXIII, 410 S. graph. Darst. 25 cm |
| ISBN: | 9781118568118 1118568117 |
Internformat
MARC
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| 100 | 1 | |a Torenbeek, Egbert |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Advanced aircraft design |b conceptual design, analysis and optimization of subsonic civil airplanes |c Egbert Torenbeek |
| 264 | 1 | |a Chichester |b Wiley |c 2013 | |
| 300 | |a XXIII, 410 S. |b graph. Darst. |c 25 cm | ||
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Datensatz im Suchindex
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| adam_text | IMAGE 1
CONTENTS
FOREWORD
SERIES PREFACE
PREFACE
ACKNOWLEDGEMENTS
1 DESIGN OF THE WELL-TEMPERED AIRCRAFT 1.1 HOW AIRCRAFT DESIGN DEVELOPED
1.1.1 EVOLUTION OF JETLINERS AND EXECUTIVE AIRCRAFT 1.1.2 A FRAMEWORK
FOR ADVANCED DESIGN
1.1.3 ANALYTICAL DESIGN OPTIMIZATION 1.1.4 COMPUTATIONAL DESIGN
ENVIRONMENT 1.2 CONCEPT FINDING 1.2.1 ADVANCED DESIGN
1.2.2 PRE-CONCEPTUAL STUDIES 1.3 PRODUCT DEVELOPMENT 1.3.1 CONCEPT
DEFINITION 1.3.2 PRELIMINARY DESIGN
1.3.3 DETAIL DESIGN 1.4 BASELINE DESIGN IN A NUTSHELL 1.4.1 BASELINE
SIZING 1.4.2 POWER PLANT
1.4.3 WEIGHT AND BALANCE 1.4.4 STRUCTURE
1.4.5 PERFORMANCE ANALYSIS 1.4.6 CLOSING THE LOOP 1.5 AUTOMATED DESIGN
SYNTHESIS 1.5.1 COMPUTATIONAL SYSTEMS REQUIREMENTS
1.5.2 EXAMPLES 1.5.3 PARAMETRIC SURVEYS 1.6 TECHNOLOGY ASSESSMENT 1.7
STRUCTURE OF THE OPTIMIZATION PROBLEM
1.7.1 ANALYSIS VERSUS SYNTHESIS 1.7.2 PROBLEM CLASSIFICATION
BIBLIOGRAPHY
XV
XIX
XXI
XXV
1
4
4
5
6
6
7
8
10 11 13 13
13 15 16 16 17
18 19 19 20 21
22 25 25 26 27
IMAGE 2
VA CONTENTS
2 EARLY CONCEPTUAL DESIGN
2.1 SCENARIO AND REQUIREMENTS 2.1.1 WHAT DRIVES A DESIGN? 2.1.2 CIVIL
AIRPLANE CATEGORIES 2.1.3 TOP LEVEL REQUIREMENTS 2.2 WEIGHT TERMINOLOGY
AND PREDICTION
2.2.1 METHOD CLASSIFICATION 2.2.2 BASIC WEIGHT COMPONENTS 2.2.3 WEIGHT
LIMITS 2.2.4 TRANSPORT CAPABILITY 2.3 THE UNITY EQUATION
2.3.1 MISSION FUEL 2.3.2 EMPTY WEIGHT 2.3.3 DESIGN WEIGHTS 2.4 RANGE
PARAMETER
2.4.1 AERODYNAMIC EFFICIENCY 2.4.2 SPECIFIC FUEL CONSUMPTION AND OVERALL
EFFICIENCY 2.4.3 BEST CRUISE SPEED 2.5 ENVIRONMENTAL ISSUES 2.5.1 ENERGY
AND PAYLOAD FUEL EFFICIENCY 2.5.2 `GREENER BY DESIGN BIBLIOGRAPHY
3 PROPULSION AND ENGINE TECHNOLOGY 3.1 PROPULSION LEADING THE WAY 3.2
BASIC CONCEPTS OF JET PROPULSION 3.2.1 TURBOJET THRUST
3.2.2 TURBOFAN THRUST 3.2.3 SPECIFIC FUEL CONSUMPTION 3.2.4 OVERALL
EFFICIENCY 3.2.5 THERMAL AND PROPULSIVE EFFICIENCY 3.2.6 GENERALIZED
PERFORMANCE 3.2.7 MACH NUMBER AND ALTITUDE EFFECTS 3.3 TURBOPROP ENGINES
3.3.1 POWER AND SPECIFIC FUEL CONSUMPTION 3.3.2 GENERALIZED PERFORMANCE
3.3.3 HIGH SPEED PROPELLERS 3.4 TURBOFAN ENGINE LAYOUT
3.4.1 BYPASS RATIO TRENDS 3.4.2 RISE AND FALL OF THE PROPFAN 3.4.3
REBIRTH OF THE OPEN ROTOR? 3.5 POWER PLANT SELECTION
3.5.1 POWER PLANT LOCATION 3.5.2 ALTERNATIVE FUELS 3.5.3 AIRCRAFT NOISE
BIBLIOGRAPHY
31 31 31 33 35
36 36 37 39 39 41 43 44 45 46 47 48 49 51 51 54 56
59 59 60 60 61 62 63 63 65 66 67 67 68 69 70 70 72 74 74 75 76 77 78
IMAGE 3
CONTENTS
4 AERODYNAMIC DRAG AND ITS REDUCTION 4.1 BASIC CONCEPTS 4.1.1 LIFT, DRAG
AND AERODYNAMIC EFFICIENCY 4.1.2 DRAG BREAKDOWN AND DEFINITIONS
4.2 DECOMPOSITION SCHEMES AND TERMINOLOGY 4.2.1 PRESSURE AND FRICTION
DRAG 4.2.2 VISCOUS DRAG 4.2.3 VORTEX DRAG
4.2.4 WAVE DRAG 4.3 SUBSONIC PARASITE AND INDUCED DRAG 4.3.1 PARASITE
DRAG 4.3.2 MONOPLANE INDUCED DRAG
4.3.3 BIPLANE INDUCED DRAG 4.3.4 MULTIPLANE AND BOXPLANE INDUCED DRAG
4.4 DRAG POLAR REPRESENTATIONS 4.4.1 TWO-TERM APPROXIMATION
4.4.2 THREE-TERM APPROXIMATION 4.4.3 REYNOLDS NUMBER EFFECTS 4.4.4
COMPRESSIBILITY CORRECTION 4.5 DRAG PREDICTION
4.5.1 INTERFERENCE DRAG 4.5.2 ROUGHNESS AND EXCRESCENCES 4.5.3
CORRECTIONS DEPENDENT ON OPERATION 4.5.4 ESTIMATION OF MAXIMUM SUBSONIC
LID
4.5.5 LOW-SPEED CONFIGURATION 4.6 VISCOUS DRAG REDUCTION 4.6.1 WETTED
AREA 4.6.2 TURBULENT FRICTION DRAG
4.6.3 NATURAL LAMINAR FLOW 4.6.4 LAMINAR FLOW CONTROL 4.6.5 HYBRID
LAMINAR FLOW CONTROL 4.6.6 GAINS, CHALLENGES AND BARRIERS OF LFC 4.7
INDUCED DRAG REDUCTION
4.7.1 WING SPAN
4.7.2 SPANWISE CAMBER 4.7.3 NON-PLANAR WING SYSTEMS BIBLIOGRAPHY
5 FROM TUBE AND WING TO FLYING WING
5.1 THE CASE FOR FLYING WINGS 5.1.1 NORTHROP S ALL-WING AIRCRAFT 5.1.2
FLYING WING CONTROVERSY 5.1.3 WHITHER ALL-WING AIRLINERS?
5.1.4 FUNDAMENTAL ISSUES 5.2 ALLOCATION OF USEFUL VOLUME 5.2.1
INTEGRATION OF THE USEFUL LOAD 5.2.2 STUDY GROUND RULES
VII
81 81 82 83
84 84 85 85
86 87 87 90 91 94 95
95 96 97 98
99 100 101 102
102 104 106 107
108 108 110 111
112 114 114 115
115 115
121 121 121 123
124 126 127 128
128
IMAGE 4
VIII
5.2.3 VOLUME RATIO 5.2.4 ZERO-LIFT DRAG 5.2.5 GENERALIZED AERODYNAMIC
EFFICIENCY 5.2.6 PARTIAL OPTIMA 5.3 SURVEY OF AERODYNAMIC EFFICIENCY
5.3.1 ALTITUDE VARIATION 5.3.2 ASPECT RATIO AND SPAN 5.3.3
ENGINE-AIRFRAME MATCHING 5.4 SURVEY OF THE PARAMETER MUD
5.4.1 OPTIMUM FLIGHT CONDITIONS 5.4.2 THE DRAG PARAMETER 5.5 INTEGRATED
CONFIGURATIONS COMPARED 5.5.1 CONVENTIONAL BASELINE
5.5.2 IS A WING ALONE SUFFICIENT? 5.5.3 BLENDED WING BODY 5.5.4 HYBRID
FLYING WING 5.5.5 SPAN LOADER 5.6 FLYING WING DESIGN
5.6.1 HANG-UPS OR SHOWSTOPPER? 5.6.2 STRUCTURAL DESIGN AND WEIGHT 5.6.3
THE FLYING WING: WILL IT FLY? BIBLIOGRAPHY
6 CLEAN SHEET DESIGN
6.1 DOMINANT AND RADICAL CONFIGURATIONS
6.2
6.2.2 6.2.3 6.2.4
6.2.5
6.1.1 ESTABLISHED CONFIGURATIONS 6.1.2 NEW PARADIGMS MORPHOLOGY OF
SHAPES 6.2.1 CLASSIFICATION
LIFTING SYSTEMS PLAN VIEW CLASSIFICATION STRUT-BRACED WINGS PROPULSION
AND CONCEPT INTEGRATION 6.3 WING AND TAIL CONFIGURATIONS
6.3.1 AERODYNAMIC LIMITS 6.3.2 THE BALANCED DESIGN 6.3.3 EVALUATION
6.3.4 RELAXED INHERENT STABILITY 6.4 AIRCRAFT FEATURING A FOREPLANE
6.4.1 CANARD CONFIGURATION 6.4.2 THREE-SURFACE AIRCRAFT 6.5 NON-PLANAR
LIFTING SYSTEMS 6.5.1 TRANSONIC BOXPLANE
6.5.2 C-WING
6.6 JOINED WING AIRCRAFT 6.6.1 STRUCTURAL PRINCIPLES AND WEIGHT 6.6.2
AERODYNAMIC ASPECTS
CONTENTS
129 130 131 132
134 134 135 136
138 138 139 140 141 143
144 146 147 149 149 150 151
152
157 157 157 159
159 160 160 162 163
164 165 165 167
168 169 169 170
172 173 173 175 177
178 179
IMAGE 5
CONTENTS
6.6.3 STABILITY AND CONTROL 6.6.4 DESIGN INTEGRATION 6.7 TWIN-FUSELAGE
AIRCRAFT 6.7.1 DESIGN INTEGRATION 6.8 HYDROGEN-FUELLED COMMERCIAL
TRANSPORTS
6.8.1 PROPERTIES OF LH2 6.8.2 FUEL SYSTEM 6.8.3 HANDLING SAFETY,
ECONOMICS AND LOGISTICS 6.9 PROMISING CONCEPTS
BIBLIOGRAPHY
7 AIRCRAFT DESIGN OPTIMIZATION 7.1 THE PERFECT DESIGN: AN ILLUSION? 7.2
ELEMENTS OF OPTIMIZATION 7.2.1 DESIGN PARAMETERS
7.2.2 OPTIMAL CONTROL AND DISCRETE-VARIABLE OPTIMIZATION 7.2.3 BASIC
TERMINOLOGY 7.2.4 SINGLE-OBJECTIVE OPTIMIZATION 7.2.5 UNCONSTRAINED
OPTIMIZER
7.2.6 . CONSTRAINED OPTIMIZER 7.3 ANALYTICAL OR NUMERICAL OPTIMIZATION?
7.3.1 ANALYTICAL APPROACH 7.3.2 MULTIVARIATE OPTIMIZATION
7.3.3 UNCONSTRAINED OPTIMIZATION 7.3.4 CONSTRAINED OPTIMIZATION 7.3.5
RESPONSE SURFACE APPROXIMATION 7.3.6 GLOBAL MODELS 7.4 LARGE
OPTIMIZATION PROBLEMS
7.4.1 CONCEPT SIZING AND EVALUATION 7.4.2 MULTIDISCIPLINARY OPTIMIZATION
7.4.3 SYSTEM DECOMPOSITION 7.4.4 MULTILEVEL OPTIMIZATION
7.4.5 MULTI-OBJECTIVE OPTIMIZATION 7.5 PRACTICAL OPTIMIZATION IN
CONCEPTUAL DESIGN 7.5.1 ARGUMENTS OF THE SCEPTIC 7.5.2 PROBLEM STRUCTURE
7.5.3 SELECTING SELECTION VARIABLES 7.5.4 DESIGN SENSITIVITY 7.5.5 THE
OBJECTIVE FUNCTION BIBLIOGRAPHY
8 THEORY OF OPTIMUM WEIGHT
8.1 WEIGHT ENGINEERING: CORE OF AIRCRAFT DESIGN 8.1.1 PREDICTION METHODS
8.1.2 USE OF STATISTICS
IX
180 181 182 185 186 187
188 189 189 190
197 197 198 198
199 200 201 202
204 206 206 207
209 210 211 212
213 213 214 215
217 218 219 219
220 220 222 222 223
229 229 230 231
IMAGE 6
X CONTENTS
8.2 DESIGN SENSITIVITY 8.2.1 PROBLEM STRUCTURE 8.2.2 SELECTION VARIABLES
8.3 JET TRANSPORT EMPTY WEIGHT
8.3.1 WEIGHT BREAKDOWN 8.3.2 WING STRUCTURE (ITEM 10) 8.3.3 FUSELAGE
STRUCTURE (ITEM 11) 8.3.4 EMPENNAGE STRUCTURE (ITEMS 12 AND 13)
8.3.5 LANDING GEAR STRUCTURE (ITEM 14) 8.3.6 POWER PLANT AND ENGINE
PYLONS (ITEMS 2 AND 15) 8.3.7 SYSTEMS, FURNISHINGS AND OPERATIONAL ITEMS
(ITEMS 3,4 AND 5) 8.3.8 OPERATING EMPTY WEIGHT: EXAMPLE 8.4 DESIGN
SENSITIVITY OF AIRFRAME DRAG
8.4.1 DRAG DECOMPOSITION 8.4.2 AERODYNAMIC EFFICIENCY 8.5 THRUST, POWER
PLANT AND FUEL WEIGHT 8.5.1 INSTALLED THRUST AND POWER PLANT WEIGHT
8.5.2 MISSION FUEL 8.5.3 PROPULSION WEIGHT PENALTY 8.5.4 WING AND
PROPULSION WEIGHT FRACTION 8.5.5 OPTIMUM WEIGHT FRACTIONS COMPARED 8.6
TAKE-OFF WEIGHT, THRUST AND FUEL EFFICIENCY
8.6.1 MAXIMUM TAKE-OFF WEIGHT 8.6.2 INSTALLED THRUST AND FUEL ENERGY
EFFICIENCY 8.6.3 UNCONSTRAINED OPTIMA COMPARED 8.6.4 RANGE FOR GIVEN
MTOW
8.6.5 EXTENDED RANGE VERSION 8.7 SUMMARY AND REFLECTION 8.7.1 WHICH
FIGURE OF MERIT? 8.7.2 CONCLUSION
8.7.3 ACCURACY BIBLIOGRAPHY
9 MATCHING ENGINES AND AIRFRAME 9.1 REQUIREMENTS AND CONSTRAINTS 9.2
CRUISE-SIZED ENGINES 9.2.1 INSTALLED TAKE-OFF THRUST
9.2.2 THE THUMBPRINT 9.3 LOW SPEED REQUIREMENTS 9.3.1 STALLING SPEED
9.3.2 TAKE-OFF CLIMB
9.3.3 APPROACH AND LANDING CLIMB 9.3.4 SECOND SEGMENT CLIMB GRADIENT 9.4
SCHEMATIC TAKE-OFF ANALYSIS 9.4.1 DEFINITIONS OF TAKE-OFF FIELD LENGTH
9.4.2 TAKE-OFF RUN
232 232 233 234
234 235 236 237 238 238 238 239 239 240 242 243 243 245 245 248
249 249 249 251
252 253 254 254 254 256 257
257
261 261 262 262 263 265 265 266 266 267
267 268 269
IMAGE 7
CONTENTS XI
9.4.3 AIRBORNE DISTANCE 9.4.4 TAKE-OFF DISTANCE 9.4.5 GENERALIZED THRUST
AND SPAN LOADING CONSTRAINT 9.4.6 MINIMUM THRUST FOR GIVEN TOFL 9.5
APPROACH AND LANDING
9.5.1 LANDING DISTANCE ANALYSIS 9.5.2 APPROACH SPEED AND WING LOADING
9.6 ENGINE SELECTION AND INSTALLATION 9.6.1 IDENTIFYING THE BEST MATCH
9.6.2 INITIAL ENGINE ASSESSMENT 9.6.3 ENGINE SELECTION BIBLIOGRAPHY
10 ELEMENTS OF AERODYNAMIC WING DESIGN 10.1 INTRODUCTION 10.1.1 PROBLEM
STRUCTURE 10.1.2 RELATION TO ENGINE SELECTION
10.2 PLANFORM GEOMETRY 10.2.1 WING AREA AND DESIGN LIFT COEFFICIENT
10.2.2 SPAN AND ASPECT RATIO 10.3 DESIGN SENSITIVITY INFORMATION
10.3.1 AERODYNAMIC EFFICIENCY 10.3.2 PROPULSION WEIGHT CONTRIBUTION
10.3.3 WING AND TAIL STRUCTURE WEIGHT 10.3.4 WING PENALTY FUNCTION AND
MTOW 10.4 SUBSONIC AIRCRAFT WING 10.4.1 PROBLEM STRUCTURE
10.4.2 UNCONSTRAINED OPTIMA 10.4.3 MINIMUM PROPULSION WEIGHT PENALTY
10.4.4 ACCURACY 10.5 CONSTRAINED OPTIMA
10.5.1 TAKE-OFF FIELD LENGTH 10.5.2 TANK VOLUME 10.5.3 WING AND TAIL
WEIGHT FRACTION 10.5.4 SELECTION OF THE DESIGN 10.6 TRANSONIC AIRCRAFT
WING
10.6.1 GEOMETRY 10.6.2 WING DRAG IN THE DESIGN CONDITION 10.6.3 MODIFIED
WING PENALTY FUNCTION 10.6.4 THICKNESS RATIO LIMIT
10.6.5 WPF AFFECTED BY SWEEP ANGLE AND THICKNESS RATIO 10.7 LIFT
COEFFICIENT AND ASPECT RATIO 10.7.1 PARTIAL OPTIMA 10.7.2 CONSTRAINTS
10.7.3 REFINING THE OPTIMIZATION
270 270 271 273 273
273 274 275 275
276 277 278
281 281 282 283 283
285 286 286 287
288 289 290 291
291 292 294 294
295 296 296 297
297 298 298 299
300 301 303 304
304 306 307
IMAGE 8
XII CONTENTS
10.8 DETAILED DESIGN 10.8.1 TAPER AND LIFT DISTRIBUTION 10.8.2 CAMBER
AND TWIST DISTRIBUTION 10.8.3 FORWARD SWEPT WING (FSW)
10.8.4 WING-TIP DEVICES 10.9 HIGH LIFT DEVICES 10.9.1 AERODYNAMIC
EFFECTS 10.9.2 DESIGN ASPECTS
BIBLIOGRAPHY
11 THE WING STRUCTURE AND ITS WEIGHT 11.1 INTRODUCTION 11.1.1 STATISTICS
CAN BE USEFUL 11.1.2 QUASI-ANALYTICAL WEIGHT PREDICTION 11.2 METHODOLOGY
11.2.1 WEIGHT BREAKDOWN AND STRUCTURAL CONCEPT 11.2.2 BASIC APPROACH
11.2.3 LOAD FACTORS 11.3 BASIC WING BOX
11.3.1 BENDING DUE TO LIFT 11.3.2 BENDING MATERIAL 11.3.3 SHEAR MATERIAL
11.3.4 IN-PLANE LOADS AND TORSION
11.3.5 RIBS
11.4 INERTIA RELIEF AND DESIGN LOADS 11.4.1 RELIEF DUE TO FIXED MASSES
11.4.2 WEIGHT-CRITICAL UL AND DESIGN WEIGHTS 11.5 NON-IDEAL WEIGHT
11.5.1 NON-TAPER, JOINTS AND FASTENERS 11.5.2 FAIL SAFETY AND DAMAGE
TOLERANCE 11.5.3 MANHOLES AND ACCESS HATCHES 11.5.4 REINFORCEMENTS,
ATTACHMENTS AND SUPPORT STRUCTURE
11.5.5 DYNAMIC OVER SWING 11.5.6 TORSIONAL STIFFNESS 11.6 SECONDARY
STRUCTURES AND MISCELLANEOUS ITEMS 11.6.1 FIXED LEADING EDGE
11.6.2 LEADING EDGE HIGH-LIFT DEVICES 11.6.3 FIXED TRAILING EDGE 11.6.4
TRAILING EDGE FLAPS 11.6.5 FLIGHT CONTROL DEVICES 11.6.6 TIP STRUCTURES
11.6.7 MISCELLANEOUS ITEMS 11.7 STRESS LEVELS IN ALUMINIUM ALLOYS 11.7.1
LOWER PANELS 11.7.2 UPPER PANELS
11.7.3 SHEAR STRESS IN SPAR WEBS
309 309 310 311 312
313 313 314 315
319 319 319 320 321 321 323 324 326 326 331 333 334 334 335 336 337 338
339 340 340 341 342 342 344 345
345 346 346
348 348 349 349 350 350 352
IMAGE 9
CONTENTS
11.8 REFINEMENTS 11.8.1 TIP EXTENSIONS 11.8.2 CENTRE SECTION 11.8.3
COMPOUND TAPER 11.8.4 EXPOSED WING LIFT 11.8.5 ADVANCED MATERIALS 11.9
APPLICATION
11.9.1 BASIC IDEAL STRUCTURE WEIGHT 11.9.2 REFINED IDEAL STRUCTURE
WEIGHT 11.9.3 WING STRUCTURE WEIGHT 11.9.4 ACCURACY
11.9.5 CONCLUSION BIBLIOGRAPHY
12 UNIFIED CRUISE PERFORMANCE 12.1 INTRODUCTION 12.1.1 CLASSICAL
SOLUTIONS 12.1.2 UNIFIED CRUISE PERFORMANCE
12.1.3 SPECIFIC RANGE AND THE RANGE PARAMETER 12.2 MAXIMUM AERODYNAMIC
EFFICIENCY 12.2.1. LOGARITHMIC DRAG DERIVATIVES 12.2.2 INTERPRETATION OF
LOG-DERIVATIVES
12.2.3 ALTITUDE CONSTRAINT 12.3 THE PARAMETER ML/D 12.3.1 SUBSONIC
FLIGHT MACH NUMBER 12.3.2 TRANSONIC FLIGHT MACH NUMBER
12.4 THE RANGE PARAMETER 12.4.1 UNCONSTRAINED OPTIMA 12.4.2 CONSTRAINED
OPTIMA 12.4.3 INTERPRETATION OF RIM 12.4.4 OPTIMUM CRUISE CONDITION 12.5
RANGE IN CRUISING FLIGHT
12.5.1 BREGUET RANGE EQUATION 12.5.2 CONTINUOUS CRUISE/CLIMB 12.5.3
HORIZONTAL CRUISE, CONSTANT SPEED 12.5.4 HORIZONTAL CRUISE, CONSTANT
LIFT COEFFICIENT 12.6 CRUISE PROCEDURES AND MISSION FUEL
12.6.1 SUBSONIC FLIGHT 12.6.2 TRANSONIC FLIGHT 12.6.3 CRUISE FUEL 12.6.4
MISSION FUEL
12.6.5 RESERVE FUEL 12.7 REFLECTION 12.7.1 SUMMARY OF RESULTS 12.7.2 THE
DESIGN CONNECTION
BIBLIOGRAPHY
XLLL
352 352 353 354
355 355 357 357 358 359
359 360 361
363 363 363 364 365
366 368 369
370 371 371 372 374 374
376 376 378
379 379 380 381
381 382 382 383 384 385 387
388 388 389 390
IMAGE 10
XIV CONTENTS
A VOLUMES, SURFACE AND WETTED AREAS A. 1 WING
A. 2 FUSELAGE A. 3 TAIL SURFACES A. 4 ENGINE NACELLES AND PYLONS A. 5
AIRFRAME WETTED AREA
BIBLIOGRAPHY
B INTERNATIONAL STANDARD ATMOSPHERE
C ABBREVIATIONS
393 393 394 395
395 395 396
397
399
INDEX 403
|
| any_adam_object | 1 |
| author | Torenbeek, Egbert |
| author_facet | Torenbeek, Egbert |
| author_role | aut |
| author_sort | Torenbeek, Egbert |
| author_variant | e t et |
| building | Verbundindex |
| bvnumber | BV041207962 |
| classification_rvk | ZO 7200 |
| classification_tum | VER 600f |
| ctrlnum | (OCoLC)855546866 (DE-599)BSZ38750608X |
| discipline | Verkehrstechnik Verkehr / Transport |
| format | Book |
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| id | DE-604.BV041207962 |
| illustrated | Illustrated |
| indexdate | 2024-07-10T00:42:06Z |
| institution | BVB |
| isbn | 9781118568118 1118568117 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-026182720 |
| oclc_num | 855546866 |
| open_access_boolean | |
| owner | DE-573 DE-91G DE-BY-TUM DE-210 DE-706 |
| owner_facet | DE-573 DE-91G DE-BY-TUM DE-210 DE-706 |
| physical | XXIII, 410 S. graph. Darst. 25 cm |
| publishDate | 2013 |
| publishDateSearch | 2013 |
| publishDateSort | 2013 |
| publisher | Wiley |
| record_format | marc |
| series2 | Aerospace Series |
| spelling | Torenbeek, Egbert Verfasser aut Advanced aircraft design conceptual design, analysis and optimization of subsonic civil airplanes Egbert Torenbeek Chichester Wiley 2013 XXIII, 410 S. graph. Darst. 25 cm txt rdacontent n rdamedia nc rdacarrier Aerospace Series Flugzeugbau (DE-588)4154782-2 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf Konstruktion (DE-588)4032231-2 gnd rswk-swf Flugzeug (DE-588)4017672-1 s Konstruktion (DE-588)4032231-2 s DE-604 Flugzeugbau (DE-588)4154782-2 s Digitalisierung Deutsches Museum application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=026182720&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Torenbeek, Egbert Advanced aircraft design conceptual design, analysis and optimization of subsonic civil airplanes Flugzeugbau (DE-588)4154782-2 gnd Flugzeug (DE-588)4017672-1 gnd Konstruktion (DE-588)4032231-2 gnd |
| subject_GND | (DE-588)4154782-2 (DE-588)4017672-1 (DE-588)4032231-2 |
| title | Advanced aircraft design conceptual design, analysis and optimization of subsonic civil airplanes |
| title_auth | Advanced aircraft design conceptual design, analysis and optimization of subsonic civil airplanes |
| title_exact_search | Advanced aircraft design conceptual design, analysis and optimization of subsonic civil airplanes |
| title_full | Advanced aircraft design conceptual design, analysis and optimization of subsonic civil airplanes Egbert Torenbeek |
| title_fullStr | Advanced aircraft design conceptual design, analysis and optimization of subsonic civil airplanes Egbert Torenbeek |
| title_full_unstemmed | Advanced aircraft design conceptual design, analysis and optimization of subsonic civil airplanes Egbert Torenbeek |
| title_short | Advanced aircraft design |
| title_sort | advanced aircraft design conceptual design analysis and optimization of subsonic civil airplanes |
| title_sub | conceptual design, analysis and optimization of subsonic civil airplanes |
| topic | Flugzeugbau (DE-588)4154782-2 gnd Flugzeug (DE-588)4017672-1 gnd Konstruktion (DE-588)4032231-2 gnd |
| topic_facet | Flugzeugbau Flugzeug Konstruktion |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=026182720&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT torenbeekegbert advancedaircraftdesignconceptualdesignanalysisandoptimizationofsubsoniccivilairplanes |