Aircraft design: a conceptual approach
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Reston, VA
American Inst. of Aeronautics and Astronautics
2006
|
| Ausgabe: | 4. ed. |
| Schriftenreihe: | AIAA education series
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Erg. durch: Raymer, Daniel P.: RDS-STUDENT |
| Beschreibung: | XIX, 838 S. Ill., graph. Darst. 24 cm |
| ISBN: | 1563478293 9781563478291 |
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Datensatz im Suchindex
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| adam_text | AIRCRAFT DESIGN: A CONCEPTUAL APPROACH FOURTH EDITION DANIEL P. RAYMER
CONCEPTUAL RESEARCH CORPORATION PLAYA DEL REY, CALIFORNIA 4AIAA
EDUCATION SERIES JOSEPH A. SCHETZ SERIES EDITOR-IN-CHIEF VIRGINIA
POLYTECHNIC INSTITUTE AND STATE UNIVERSITY BLACKSBURG, VIRGINIA
PUBLISHED BY THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS,
INC. 1801 ALEXANDER BELL DRIVE, RESTON, VIRGINIA 20191-4344 TABLE OF
CONTENTS PREFACE XVII AUTHOR S NOTE CONCERNING USE OF METRIC WEIGHT
UNITS XIX 1. DESIGN*A SEPARATE DISCIPLINE 1 1.1 WHAT IS DESIGN? 1 1.2
INTRODUCTION TO THE BOOK 1 2. OVERVIEW OF THE DESIGN PROCESS 3 2.1
INTRODUCTION 3 2.2 PHASES OF AIRCRAFT DESIGN 3 2.3 AIRCRAFT CONCEPTUAL
DESIGN PROCESS 8 2.4 INTEGRATED PRODUCT DEVELOPMENT AND AIRCRAFT DESIGN
12 3. SIZING FROM A CONCEPTUAL SKETCH 15 3.1 INTRODUCTION 15 3.2
TAKEOFF-WEIGHT BUILDUP 16 3.3 EMPTY-WEIGHT ESTIMATION 16 3.4
FUEL-FRACTION ESTIMATION 18 3.5 TAKEOFF-WEIGHT CALCULATION 27 3.6 DESIGN
EXAMPLE: ASW AIRCRAFT 28 4. AIRFOIL AND GEOMETRY SELECTION 37 4.1
INTRODUCTION 37 4.2 AIRFOIL SELECTION 37 4.3 WING GEOMETRY 51 4.4
BIPLANE WINGS 71 4.5 TAIL GEOMETRY AND ARRANGEMENT 73 5.
THRUST-TO-WEIGHT RATIO AND WING LOADING 87 5.1 INTRODUCTION 87 5.2
THRUST-TO-WEIGHT RATIO 88 5.3 WING LOADING 94 5.4 SELECTION OF THRUST TO
WEIGHT AND WING LOADING 110 XI XII 6. INITIAL SIZING ILL 6.1
INTRODUCTION ILL 6.2 RUBBER VS FIXED-SIZE ENGINES ILL 6.3
RUBBER-ENGINE SIZING 112 6.4 FIXED-ENGINE SIZING 118 6.5 GEOMETRY SIZING
119 6.6 CONTROL-SURFACE SIZING 123 7. CONFIGURATION LAYOUT AND LOFT 127
7.1 INTRODUCTION 127 7.2 END PRODUCTS OF CONFIGURATION LAYOUT 127 7.3
CONIC LOFTING 132 7.4 CONIC FUSELAGE DEVELOPMENT 138 7.5 FLAT-WRAP
FUSELAGE LOFTING 146 7.6 CIRCLE-TO-SQUARE ADAPTER 147 7.7 FUSELAGE LOFT
VERIFICATION 148 7.8 WING/TAIL LAYOUT AND LOFT 149 7.9 WETTED AREA
DETERMINATION 161 7.10 VOLUME DETERMINATION 163 7.11 USE OF
COMPUTER-AIDED DESIGN (CAD) IN CONCEPTUAL DESIGN. ... 164 8. SPECIAL
CONSIDERATIONS IN CONFIGURATION LAYOUT 169 8.1 INTRODUCTION 169 8.2
AERODYNAMIC CONSIDERATIONS 169 8.3 STRUCTURAL CONSIDERATIONS 177 8.4
RADAR DETECTABILITY 185 8.5 INFRARED DETECTABILITY 195 8.6 VISUAL
DETECTABILITY 196 8.7 AURAL SIGNATURE 197 8.8 VULNERABILITY
CONSIDERATIONS 197 8.9 CRASHWORTHINESS CONSIDERATIONS 199 8.10
PRODUCIBILITY CONSIDERATIONS 201 8.11 MAINTAINABILITY CONSIDERATIONS 205
9. CREW STATION, PASSENGERS, AND PAYLOAD 209 9.1 INTRODUCTION 209 9.2
CREW STATION 209 9.3 PASSENGER COMPARTMENT 213 9.4 CARGO PROVISIONS 214
9.5 WEAPONS CARRIAGE 216 9.6 GUN INSTALLATION 219 10. PROPULSION AND
FUEL SYSTEM INTEGRATION 221 10.1 INTRODUCTION 221 10.2 PROPULSION
SELECTION 221 10.3 JET-ENGINE INTEGRATION *. 224 10.4 PROPELLER-ENGINE
INTEGRATION 250 10.5 FUEL SYSTEM 257 XIII 11. LANDING GEAR AND
SUBSYSTEMS 261 11.1 INTRODUCTION 261 11.2 LANDING GEAR ARRANGEMENTS 261
11.3 TIRE SIZING 266 11.4 SHOCK ABSORBERS 272 11.5 CASTORING-WHEEL
GEOMETRY 279 11.6 GEAR-RETRACTION GEOMETRY 280 11.7 SEAPLANES 283 11.8
SUBSYSTEMS 285 INTERMISSION: STEP-BY-STEP DEVELOPMENT OF A NEW DESIGN
295 12. AERODYNAMICS 303 12.1 INTRODUCTION 303 12.2 AERODYNAMIC FORCES
304 12.3 AERODYNAMIC COEFFICIENTS 308 12.4 LIFT 309 12.5 PARASITE
(ZERO-LIFT) DRAG 327 12.6 DRAG DUE TO LIFT (INDUCED DRAG) 346 12.7
AERODYNAMIC CODES AND COMPUTATIONAL FLUID DYNAMICS (CFD) 354 13.
PROPULSION 365 13.1 INTRODUCTION 365 13.2 JET-ENGINE THRUST
CONSIDERATIONS 367 13.3 TURBOJET INSTALLED THRUST 370 13.4 THRUST-DRAG
BOOKKEEPING 370 13.5 INSTALLED-THRUST METHODOLOGY 371 13.6 PISTON-ENGINE
PERFORMANCE 379 13.7 TURBOPROP PERFORMANCE 386 14. STRUCTURES AND LOADS
389 14.1 INTRODUCTION 389 14.2 LOADS CATEGORIES 390 14.3 AIR LOADS 392
14.4 INERTIAL LOADS 402 14.5 POWERPLANT LOADS 402 14.6 LANDING-GEAR
LOADS 402 14.7 STRUCTURES FUNDAMENTALS 403 14.8 MATERIAL SELECTION 408
14.9 MATERIAL PROPERTIES 413 14.10 STRUCTURAL-ANALYSIS FUNDAMENTALS 425
14.11 FINITE ELEMENT STRUCTURAL ANALYSIS 443 15. WEIGHTS 451 15.1
INTRODUCTION 451 15.2 APPROXIMATE GROUP WEIGHTS METHOD 454 XIV 15.3
STATISTICAL GROUP WEIGHTS METHOD 454 15.4 ADDITIONAL CONSIDERATIONS IN
WEIGHTS ESTIMATION 463 16. STABILITY, CONTROL, AND HANDLING QUALITIES
467 16.1 INTRODUCTION 467 16.2 COORDINATE SYSTEMS AND DEFINITIONS 469
16.3 LONGITUDINAL STATIC STABILITY AND CONTROL 470 16.4
LATERAL-DIRECTIONAL STATIC STABILITY AND CONTROL 490 16.5 STICK-FREE
STABILITY 499 16.6 EFFECTS OF FLEXIBILITY 499 16.7 DYNAMIC STABILITY 501
16.8 QUASI STEADY STATE 505 16.9 INERTIA COUPLING 506 16.10 HANDLING
QUALITIES 508 17. PERFORMANCE AND FLIGHT MECHANICS 515 17.1 INTRODUCTION
AND EQUATIONS OF MOTION 515 17.2 STEADY LEVEL FLIGHT 516 17.3 STEADY
CLIMBING AND DESCENDING FLIGHT 525 17.4 LEVEL TURNING FLIGHT 529 17.5
GLIDING FLIGHT 532 17.6 ENERGY-MANEUVERABILITY METHODS 536 17.7
OPERATING ENVELOPE 544 17.8 TAKEOFF ANALYSIS 546 17.9 LANDING ANALYSIS
550 17.10 OTHER FIGHTER PERFORMANCE MEASURES OF MERIT 552 18. COST
ANALYSIS 561 18.1 INTRODUCTION 561 18.2 ELEMENTS OF LIFE-CYCLE COST 562
18.3 COST-ESTIMATING METHODS 565 18.4 RDT&E AND PRODUCTION COSTS 566
18.5 OPERATIONS AND MAINTENANCE COSTS 570 18.6 COST MEASURES OF MERIT
(MILITARY) 574 18.7 AIRCRAFT AND AIRLINE ECONOMICS 575 19. SIZING AND
TRADE STUDIES 579 19.1 INTRODUCTION 579 19.2 DETAILED SIZING METHODS 579
19.3 IMPROVED CONCEPTUAL SIZING METHODS 580 19.4 SIZING MATRIX AND
CARPET PLOTS 585 19.5 TRADE STUDIES 591 20. VERTICAL FLIGHT*JET AND PROP
599 20.1 INTRODUCTION 599 20.2 JET VTOL 599 20.3 PROP VTOL AND
HELICOPTER 619 XV 21. EXTREMES OF FLIGHT 637 21.1 INTRODUCTION 637 21.2
ROCKETS, LAUNCH VEHICLES, AND SPACECRAFT 637 21.3 HYPERSONIC VEHICLES
649 21.4 LIGHTER-THAN-AIR 652 22. DESIGN OF UNIQUE AIRCRAFT CONCEPTS 661
22.1 INTRODUCTION 661 22.2 FLYING WING, TAILLESS, LIFTING FUSELAGE, AND
BLENDED WING BODY. 661 22.3 DELTA AND DOUBLE-DELTA WING 666 22.4
FORWARD-SWEPT WING 667 22.5 CANARD-PUSHER 669 22.6 MULTI-FUSELAGE . 670
22.7 ASYMMETRICAL 672 22.8 JOINED WING 676 22.9 WING-IN-GROUND EFFECT
678 22.10 UNMANNED/UNINHABITED 679 23. CONCEPTUAL DESIGN EXAMPLES 683
23.1 INTRODUCTION 683 23.2 SINGLE-SEAT AEROBATIC 684 23.3 LIGHTWEIGHT
SUPERCRUISE FIGHTER 721 APPENDIX A. UNIT CONVERSION 775 APPENDIX B.
STANDARD ATMOSPHERE 777 APPENDIX C. AIRSPEED 781 APPENDIX D. AIRFOIL
DATA 783 APPENDIX E. TYPICAL ENGINE PERFORMANCE CURVES 795 E.I
AFTERBURNING TURBOFAN 795 E.2 HIGH-BYPASS TURBOFAN 799 E.3 TURBOPROP 801
APPENDIX F. DESIGN REQUIREMENTS AND SPECIFICATIONS 803 QUESTIONS 807
REFERENCES 817 INDEX 825 SUPPORTING MATERIALS 839
|
| adam_txt |
AIRCRAFT DESIGN: A CONCEPTUAL APPROACH FOURTH EDITION DANIEL P. RAYMER
CONCEPTUAL RESEARCH CORPORATION PLAYA DEL REY, CALIFORNIA 4AIAA
EDUCATION SERIES JOSEPH A. SCHETZ SERIES EDITOR-IN-CHIEF VIRGINIA
POLYTECHNIC INSTITUTE AND STATE UNIVERSITY BLACKSBURG, VIRGINIA
PUBLISHED BY THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS,
INC. 1801 ALEXANDER BELL DRIVE, RESTON, VIRGINIA 20191-4344 TABLE OF
CONTENTS PREFACE XVII AUTHOR'S NOTE CONCERNING USE OF METRIC WEIGHT
UNITS XIX 1. DESIGN*A SEPARATE DISCIPLINE 1 1.1 WHAT IS DESIGN? 1 1.2
INTRODUCTION TO THE BOOK 1 2. OVERVIEW OF THE DESIGN PROCESS 3 2.1
INTRODUCTION 3 2.2 PHASES OF AIRCRAFT DESIGN 3 2.3 AIRCRAFT CONCEPTUAL
DESIGN PROCESS 8 2.4 INTEGRATED PRODUCT DEVELOPMENT AND AIRCRAFT DESIGN
12 3. SIZING FROM A CONCEPTUAL SKETCH 15 3.1 INTRODUCTION 15 3.2
TAKEOFF-WEIGHT BUILDUP 16 3.3 EMPTY-WEIGHT ESTIMATION 16 3.4
FUEL-FRACTION ESTIMATION 18 3.5 TAKEOFF-WEIGHT CALCULATION 27 3.6 DESIGN
EXAMPLE: ASW AIRCRAFT 28 4. AIRFOIL AND GEOMETRY SELECTION 37 4.1
INTRODUCTION 37 4.2 AIRFOIL SELECTION 37 4.3 WING GEOMETRY 51 4.4
BIPLANE WINGS 71 4.5 TAIL GEOMETRY AND ARRANGEMENT 73 5.
THRUST-TO-WEIGHT RATIO AND WING LOADING 87 5.1 INTRODUCTION 87 5.2
THRUST-TO-WEIGHT RATIO 88 5.3 WING LOADING 94 5.4 SELECTION OF THRUST TO
WEIGHT AND WING LOADING 110 XI XII 6. INITIAL SIZING ILL 6.1
INTRODUCTION ILL 6.2 "RUBBER" VS "FIXED-SIZE" ENGINES ILL 6.3
RUBBER-ENGINE SIZING 112 6.4 FIXED-ENGINE SIZING 118 6.5 GEOMETRY SIZING
119 6.6 CONTROL-SURFACE SIZING 123 7. CONFIGURATION LAYOUT AND LOFT 127
7.1 INTRODUCTION 127 7.2 END PRODUCTS OF CONFIGURATION LAYOUT 127 7.3
CONIC LOFTING 132 7.4 CONIC FUSELAGE DEVELOPMENT 138 7.5 FLAT-WRAP
FUSELAGE LOFTING 146 7.6 CIRCLE-TO-SQUARE ADAPTER 147 7.7 FUSELAGE LOFT
VERIFICATION 148 7.8 WING/TAIL LAYOUT AND LOFT 149 7.9 WETTED AREA
DETERMINATION 161 7.10 VOLUME DETERMINATION 163 7.11 USE OF
COMPUTER-AIDED DESIGN (CAD) IN CONCEPTUAL DESIGN. . 164 8. SPECIAL
CONSIDERATIONS IN CONFIGURATION LAYOUT 169 8.1 INTRODUCTION 169 8.2
AERODYNAMIC CONSIDERATIONS 169 8.3 STRUCTURAL CONSIDERATIONS 177 8.4
RADAR DETECTABILITY 185 8.5 INFRARED DETECTABILITY 195 8.6 VISUAL
DETECTABILITY 196 8.7 AURAL SIGNATURE 197 8.8 VULNERABILITY
CONSIDERATIONS 197 8.9 CRASHWORTHINESS CONSIDERATIONS 199 8.10
PRODUCIBILITY CONSIDERATIONS 201 8.11 MAINTAINABILITY CONSIDERATIONS 205
9. CREW STATION, PASSENGERS, AND PAYLOAD 209 9.1 INTRODUCTION 209 9.2
CREW STATION 209 9.3 PASSENGER COMPARTMENT 213 9.4 CARGO PROVISIONS 214
9.5 WEAPONS CARRIAGE 216 9.6 GUN INSTALLATION 219 10. PROPULSION AND
FUEL SYSTEM INTEGRATION 221 10.1 INTRODUCTION 221 10.2 PROPULSION
SELECTION 221 10.3 JET-ENGINE INTEGRATION *. 224 10.4 PROPELLER-ENGINE
INTEGRATION 250 10.5 FUEL SYSTEM 257 XIII 11. LANDING GEAR AND
SUBSYSTEMS 261 11.1 INTRODUCTION 261 11.2 LANDING GEAR ARRANGEMENTS 261
11.3 TIRE SIZING 266 11.4 SHOCK ABSORBERS 272 11.5 CASTORING-WHEEL
GEOMETRY 279 11.6 GEAR-RETRACTION GEOMETRY 280 11.7 SEAPLANES 283 11.8
SUBSYSTEMS 285 INTERMISSION: STEP-BY-STEP DEVELOPMENT OF A NEW DESIGN
295 12. AERODYNAMICS 303 12.1 INTRODUCTION 303 12.2 AERODYNAMIC FORCES
304 12.3 AERODYNAMIC COEFFICIENTS 308 12.4 LIFT 309 12.5 PARASITE
(ZERO-LIFT) DRAG 327 12.6 DRAG DUE TO LIFT (INDUCED DRAG) 346 12.7
AERODYNAMIC CODES AND COMPUTATIONAL FLUID DYNAMICS (CFD) 354 13.
PROPULSION 365 13.1 INTRODUCTION 365 13.2 JET-ENGINE THRUST
CONSIDERATIONS 367 13.3 TURBOJET INSTALLED THRUST 370 13.4 THRUST-DRAG
BOOKKEEPING 370 13.5 INSTALLED-THRUST METHODOLOGY 371 13.6 PISTON-ENGINE
PERFORMANCE 379 13.7 TURBOPROP PERFORMANCE 386 14. STRUCTURES AND LOADS
389 14.1 INTRODUCTION 389 14.2 LOADS CATEGORIES 390 14.3 AIR LOADS 392
14.4 INERTIAL LOADS 402 14.5 POWERPLANT LOADS 402 14.6 LANDING-GEAR
LOADS 402 14.7 STRUCTURES FUNDAMENTALS 403 14.8 MATERIAL SELECTION 408
14.9 MATERIAL PROPERTIES 413 14.10 STRUCTURAL-ANALYSIS FUNDAMENTALS 425
14.11 FINITE ELEMENT STRUCTURAL ANALYSIS 443 15. WEIGHTS 451 15.1
INTRODUCTION 451 15.2 APPROXIMATE GROUP WEIGHTS METHOD 454 XIV 15.3
STATISTICAL GROUP WEIGHTS METHOD 454 15.4 ADDITIONAL CONSIDERATIONS IN
WEIGHTS ESTIMATION 463 16. STABILITY, CONTROL, AND HANDLING QUALITIES
467 16.1 INTRODUCTION 467 16.2 COORDINATE SYSTEMS AND DEFINITIONS 469
16.3 LONGITUDINAL STATIC STABILITY AND CONTROL 470 16.4
LATERAL-DIRECTIONAL STATIC STABILITY AND CONTROL 490 16.5 STICK-FREE
STABILITY 499 16.6 EFFECTS OF FLEXIBILITY 499 16.7 DYNAMIC STABILITY 501
16.8 QUASI STEADY STATE 505 16.9 INERTIA COUPLING 506 16.10 HANDLING
QUALITIES 508 17. PERFORMANCE AND FLIGHT MECHANICS 515 17.1 INTRODUCTION
AND EQUATIONS OF MOTION 515 17.2 STEADY LEVEL FLIGHT 516 17.3 STEADY
CLIMBING AND DESCENDING FLIGHT 525 17.4 LEVEL TURNING FLIGHT 529 17.5
GLIDING FLIGHT 532 17.6 ENERGY-MANEUVERABILITY METHODS 536 17.7
OPERATING ENVELOPE 544 17.8 TAKEOFF ANALYSIS 546 17.9 LANDING ANALYSIS
550 17.10 OTHER FIGHTER PERFORMANCE MEASURES OF MERIT 552 18. COST
ANALYSIS 561 18.1 INTRODUCTION 561 18.2 ELEMENTS OF LIFE-CYCLE COST 562
18.3 COST-ESTIMATING METHODS 565 18.4 RDT&E AND PRODUCTION COSTS 566
18.5 OPERATIONS AND MAINTENANCE COSTS 570 18.6 COST MEASURES OF MERIT
(MILITARY) 574 18.7 AIRCRAFT AND AIRLINE ECONOMICS 575 19. SIZING AND
TRADE STUDIES 579 19.1 INTRODUCTION 579 19.2 DETAILED SIZING METHODS 579
19.3 IMPROVED CONCEPTUAL SIZING METHODS 580 19.4 SIZING MATRIX AND
CARPET PLOTS 585 19.5 TRADE STUDIES 591 20. VERTICAL FLIGHT*JET AND PROP
599 20.1 INTRODUCTION 599 20.2 JET VTOL 599 20.3 PROP VTOL AND
HELICOPTER 619 XV 21. EXTREMES OF FLIGHT 637 21.1 INTRODUCTION 637 21.2
ROCKETS, LAUNCH VEHICLES, AND SPACECRAFT 637 21.3 HYPERSONIC VEHICLES
649 21.4 LIGHTER-THAN-AIR 652 22. DESIGN OF UNIQUE AIRCRAFT CONCEPTS 661
22.1 INTRODUCTION 661 22.2 FLYING WING, TAILLESS, LIFTING FUSELAGE, AND
BLENDED WING BODY. 661 22.3 DELTA AND DOUBLE-DELTA WING 666 22.4
FORWARD-SWEPT WING 667 22.5 CANARD-PUSHER 669 22.6 MULTI-FUSELAGE .' 670
22.7 ASYMMETRICAL 672 22.8 JOINED WING 676 22.9 WING-IN-GROUND EFFECT
678 22.10 UNMANNED/UNINHABITED 679 23. CONCEPTUAL DESIGN EXAMPLES 683
23.1 INTRODUCTION 683 23.2 SINGLE-SEAT AEROBATIC 684 23.3 LIGHTWEIGHT
SUPERCRUISE FIGHTER 721 APPENDIX A. UNIT CONVERSION 775 APPENDIX B.
STANDARD ATMOSPHERE 777 APPENDIX C. AIRSPEED 781 APPENDIX D. AIRFOIL
DATA 783 APPENDIX E. TYPICAL ENGINE PERFORMANCE CURVES 795 E.I
AFTERBURNING TURBOFAN 795 E.2 HIGH-BYPASS TURBOFAN 799 E.3 TURBOPROP 801
APPENDIX F. DESIGN REQUIREMENTS AND SPECIFICATIONS 803 QUESTIONS 807
REFERENCES 817 INDEX 825 SUPPORTING MATERIALS 839 |
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| callnumber-subject | TL - Motor Vehicles and Aeronautics |
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| discipline | Verkehrstechnik Verkehr / Transport |
| discipline_str_mv | Verkehrstechnik Verkehr / Transport |
| edition | 4. ed. |
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| genre | 1\p (DE-588)4123623-3 Lehrbuch gnd-content |
| genre_facet | Lehrbuch |
| id | DE-604.BV021789806 |
| illustrated | Illustrated |
| index_date | 2024-07-02T15:44:12Z |
| indexdate | 2024-07-09T20:44:40Z |
| institution | BVB |
| isbn | 1563478293 9781563478291 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-015002472 |
| oclc_num | 64084334 |
| open_access_boolean | |
| owner | DE-91G DE-BY-TUM DE-Aug4 DE-210 DE-83 DE-573 |
| owner_facet | DE-91G DE-BY-TUM DE-Aug4 DE-210 DE-83 DE-573 |
| physical | XIX, 838 S. Ill., graph. Darst. 24 cm |
| publishDate | 2006 |
| publishDateSearch | 2006 |
| publishDateSort | 2006 |
| publisher | American Inst. of Aeronautics and Astronautics |
| record_format | marc |
| series2 | AIAA education series |
| spelling | Raymer, Daniel P. Verfasser aut Aircraft design a conceptual approach Daniel P. Raymer 4. ed. Reston, VA American Inst. of Aeronautics and Astronautics 2006 XIX, 838 S. Ill., graph. Darst. 24 cm txt rdacontent n rdamedia nc rdacarrier AIAA education series Erg. durch: Raymer, Daniel P.: RDS-STUDENT Avions - Conception et construction Airplanes Design and construction Konstruktion (DE-588)4032231-2 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf Entwurf (DE-588)4121208-3 gnd rswk-swf Flugzeugbau (DE-588)4154782-2 gnd rswk-swf 1\p (DE-588)4123623-3 Lehrbuch gnd-content Flugzeugbau (DE-588)4154782-2 s Entwurf (DE-588)4121208-3 s Konstruktion (DE-588)4032231-2 s DE-604 Flugzeug (DE-588)4017672-1 s 2\p DE-604 HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015002472&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 2\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
| spellingShingle | Raymer, Daniel P. Aircraft design a conceptual approach Avions - Conception et construction Airplanes Design and construction Konstruktion (DE-588)4032231-2 gnd Flugzeug (DE-588)4017672-1 gnd Entwurf (DE-588)4121208-3 gnd Flugzeugbau (DE-588)4154782-2 gnd |
| subject_GND | (DE-588)4032231-2 (DE-588)4017672-1 (DE-588)4121208-3 (DE-588)4154782-2 (DE-588)4123623-3 |
| title | Aircraft design a conceptual approach |
| title_auth | Aircraft design a conceptual approach |
| title_exact_search | Aircraft design a conceptual approach |
| title_exact_search_txtP | Aircraft design a conceptual approach |
| title_full | Aircraft design a conceptual approach Daniel P. Raymer |
| title_fullStr | Aircraft design a conceptual approach Daniel P. Raymer |
| title_full_unstemmed | Aircraft design a conceptual approach Daniel P. Raymer |
| title_short | Aircraft design |
| title_sort | aircraft design a conceptual approach |
| title_sub | a conceptual approach |
| topic | Avions - Conception et construction Airplanes Design and construction Konstruktion (DE-588)4032231-2 gnd Flugzeug (DE-588)4017672-1 gnd Entwurf (DE-588)4121208-3 gnd Flugzeugbau (DE-588)4154782-2 gnd |
| topic_facet | Avions - Conception et construction Airplanes Design and construction Konstruktion Flugzeug Entwurf Flugzeugbau Lehrbuch |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015002472&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT raymerdanielp aircraftdesignaconceptualapproach |