Introduction to aeronautics: a design perspective
Saved in:
| Format: | Book |
|---|---|
| Language: | English |
| Published: |
Reston, Va.
American Inst. of Aeronautics and Astronautics
2004
|
| Edition: | 2. ed. |
| Series: | AIAA education series
|
| Subjects: | |
| Online Access: | Inhaltsverzeichnis |
| Physical Description: | XXII, 509 S. Ill., graph. Darst. |
| ISBN: | 1563477017 |
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Record in the Search Index
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| adam_text | INTRODUCTION TO AERONAUTICS: A DESIGN PERSPECTIVE SECOND EDITION STEVEN
A. BRANDT U.S. AIR FORCE ACADEMY COLORADO SPRINGS, COLORADO RANDALL J.
STILES COLORADO COLLEGE COLORADO SPRINGS, COLORADO JOHN J. BERTIN U.S.
AIR FORCE ACADEMY COLORADO SPRINGS, COLORADO RAY WHITFORD ROYAL MILITARY
COLLEGE OF SCIENCE AND THE CRANFIELD INSTITUTE OF TECHNOLOGY UNITED
KINGDOM EDUCATION SERIES JOSEPH A. SCHETZ SERIES EDITOR-IN-CHIEF
VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY BLACKSBURG, VIRGINIA
PUBLISHED BY AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS, INC.
1801 ALEXANDER BELL DRIVE, RESTON, VA 20191-4344 TABLE OF CONTENTS
PREFACE XV ACKNOWLEDGMENTS XVII NOMENCLATURE XIX CHAPTER 1. DESIGN
THINKING 1 1.1 INTRODUCTION 1 1.2 DESIGN METHOD 1 1.3 DESIGN EXAMPLE 6
1.4 DESIGN AND AERONAUTICS 11 1.5 BRIEF HISTORY OF AIRCRAFT DESIGN 15
1.6 CONCLUSION 24 1.7 CHAPTER SUMMARY 24 1.8 MORE DETAILS 26 REFERENCES
36 PROBLEMS 36 CHAPTER 2. OPERATING ENVIRONMENT 41 2.1 DESIGN MOTIVATION
41 2.2 CHARACTERISTICS OF THE ATMOSPHERE 42 2.3 PRESSURE MEASUREMENT 44
2.4 STANDARD ATMOSPHERE 46 2.5 COMMON USES OF THE STANDARD ATMOSPHERE 51
2.6 CHAPTER SUMMARY 52 2.7 MORE DETAILS*MOLECULAR COLLISIONS AND
AERODYNAMICS 54 REFERENCE 57 PROBLEMS 57 CHAPTER 3. AERODYNAMICS AND
AIRFOILS 61 3.1 DESIGN MOTIVATION 61 3.2 BASIC AERODYNAMICS 61 3.3 BASIC
AERODYNAMICS APPLICATIONS 66 3.4 VISCOUS FLOW 77 3.5 AIRFOIL
CHARACTERISTICS 85 3.6 CHAPTER SUMMARY 95 3.7 MORE DETAILS 100
REFERENCES 106 PROBLEMS 106 XII CHAPTER 4. WINGS AND AIRPLANES 113 4.1
DESIGN MOTIVATION 113 4.2 WINGS 114 4.3 HIGH-LIFT DEVICES 124 4.4 WHOLE
AIRCRAFT LIFT 128 4.5 WHOLE AIRCRAFT DRAG AND DRAG POLAR 128 4.6
MACH-NUMBER EFFECTS 132 4.7 CHAPTER SUMMARY 143 4.8 MORE DETAILS 150 4.9
WHOLE AIRCRAFT ANALYSIS EXAMPLE 162 REFERENCES 169 PROBLEMS 170 CHAPTER
5. PERFORMANCE 173 5.1 DESIGN MOTIVATION 173 5.2 EQUATIONS OF MOTION 173
5.3 PROPULSION 175 5.4 DRAG CURVES 188 5.5 LIFT-TO-DRAG RATIO 191 5.6
POWER CURVES 192 5.7 CURVE SHIFTS 193 5.8 GLIDES 195 5.9 CLIMBS 198 5.10
RANGE AND ENDURANCE 201 5.11 TAKEOFF AND LANDING 217 5.12 TURNS 224 5.13
V-N DIAGRAMS 231 5.14 ENERGY HEIGHT AND SPECIFIC EXCESS POWER 233 5.15
CHAPTER SUMMARY 238 5.16 MORE DETAILS*MANEUVERABILITY DIAGRAMS AND
CONSTRAINT ANALYSIS 246 5.17 PERFORMANCE ANALYSIS EXAMPLE 253 REFERENCES
260 PROBLEMS 260 CHAPTER 6. STABILITY AND CONTROL 267 6.1 DESIGN
MOTIVATION 267 6.2 LANGUAGE 267 6.3 LONGITUDINAL CONTROL ANALYSIS / 275
6.4 LONGITUDINAL STABILITY 278 6.5 DYNAMIC LONGITUDINAL STABILITY 285
6.6 LATERAL-DIRECTIONAL STABILITY 287 6.7 DYNAMIC LATERAL-DIRECTIONAL
STABILITY 293 6.8 CHAPTER SUMMARY 295 6.9 MORE DETAILS*CALCULATING
STABILITY PARAMETERS 300 6.10 STABILITY AND CONTROL ANALYSIS EXAMPLE:
F-16A AND F-16C 305 REFERENCE 311 PROBLEMS 311 XIII CHAPTER 7.
STRUCTURES 315 7.1 DESIGN MOTIVATION 315 7.2 SOLID MECHANICS 315 7.3
TYPES OF STRESS 321 7.4 LOADS 323 7.5 STRUCTURAL LAYOUT 328 7.6
MATERIALS 331 7.7 COMPONENT SIZING 332 7.8 STRUCTURAL SIZING EXAMPLE 339
7.9 WEIGHT ESTIMATES 340 7.10 FINITE ELEMENT ANALYSIS 340 7.11 CHAPTER
SUMMARY 341 REFERENCES 342 PROBLEMS 342 CHAPTER 8. SIZING 345 8.1 DESIGN
MOTIVATION 345 8.2 INTERNAL LAYOUT 346 8.3 STRUCTURES AND WEIGHT 347 8.4
GEOMETRY CONSTRAINTS 350 8.5 MISSION ANALYSIS 354 8.6 SIZING EQUATION
362 8.7 WEIGHT FRACTION METHOD 364 8.8 WEIGHT AND BALANCE 365 8.9
MISSION ANALYSIS AND SIZING EXAMPLE 367 8.10 AERODYNAMIC 373 8.11 COST
373 8.12 CHAPTER SUMMARY 375 REFERENCES 377 PROBLEMS 378 CHAPTER 9.
PUTTING IT ALL TOGETHER: CONCEPTUAL AIRCRAFT DESIGN .... 379 9.1
INTRODUCTION 379 9.2 OVERVIEW OF THE 12 ACTIVITIES 380 9.3 CUSTOMER
FOCUS 381 9.4 DESIGN SYNTHESIS 382 9.5 GEOMETRY MODELING AND ENGINEERING
DRAWING 383 9.6 AERODYNAMIC ANALYSIS 383 9.7 PROPULSION ANALYSIS 386 9.8
CONSTRAINT ANALYSIS 387 9.9 MISSION ANALYSIS 389 9.10 WEIGHT ANALYSIS
390 9.11 SIZING 391 9.12 COST ANALYSIS 392 9.13 OPTIMIZATION 392 9.14
PERFORMANCE REPORTING 393 9.15 PUTTING IT ALL TOGETHER 393 REFERENCES
395 XIV CHAPTER 10. CASE STUDIES AND FUTURE AIRCRAFT DESIGNS 397 10.1
INTRODUCTION 397 10.2 CASE STUDY 1: 1903 WRIGHT FLYER 398 10.3 CASE
STUDY 2: DOUGLAS DC-3 403 10.4 CASE STUDY 3: EVOLUTION OF THE F-16 419
10.5 OPPORTUNITIES IN AIRCRAFT DESIGN 427 10.6 DESIGN THINKING IN OTHER
CONTEXTS 433 REFERENCES 434 APPENDIX A: GLOSSARY 437 APPENDIX B:
SUPPLEMENTAL DATA 449 APPENDIX C: ANSWERS 493 INDEX 503 SUPPORTING
MATERIALS 509
|
| adam_txt |
INTRODUCTION TO AERONAUTICS: A DESIGN PERSPECTIVE SECOND EDITION STEVEN
A. BRANDT U.S. AIR FORCE ACADEMY COLORADO SPRINGS, COLORADO RANDALL J.
STILES COLORADO COLLEGE COLORADO SPRINGS, COLORADO JOHN J. BERTIN U.S.
AIR FORCE ACADEMY COLORADO SPRINGS, COLORADO RAY WHITFORD ROYAL MILITARY
COLLEGE OF SCIENCE AND THE CRANFIELD INSTITUTE OF TECHNOLOGY UNITED
KINGDOM EDUCATION SERIES JOSEPH A. SCHETZ SERIES EDITOR-IN-CHIEF
VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY BLACKSBURG, VIRGINIA
PUBLISHED BY AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS, INC.
1801 ALEXANDER BELL DRIVE, RESTON, VA 20191-4344 TABLE OF CONTENTS
PREFACE XV ACKNOWLEDGMENTS XVII NOMENCLATURE XIX CHAPTER 1. DESIGN
THINKING 1 1.1 INTRODUCTION 1 1.2 DESIGN METHOD 1 1.3 DESIGN EXAMPLE 6
1.4 DESIGN AND AERONAUTICS 11 1.5 BRIEF HISTORY OF AIRCRAFT DESIGN 15
1.6 CONCLUSION 24 1.7 CHAPTER SUMMARY 24 1.8 MORE DETAILS 26 REFERENCES
36 PROBLEMS 36 CHAPTER 2. OPERATING ENVIRONMENT 41 2.1 DESIGN MOTIVATION
41 2.2 CHARACTERISTICS OF THE ATMOSPHERE 42 2.3 PRESSURE MEASUREMENT 44
2.4 STANDARD ATMOSPHERE 46 2.5 COMMON USES OF THE STANDARD ATMOSPHERE 51
2.6 CHAPTER SUMMARY 52 2.7 MORE DETAILS*MOLECULAR COLLISIONS AND
AERODYNAMICS 54 REFERENCE 57 PROBLEMS 57 CHAPTER 3. AERODYNAMICS AND
AIRFOILS 61 3.1 DESIGN MOTIVATION 61 3.2 BASIC AERODYNAMICS 61 3.3 BASIC
AERODYNAMICS APPLICATIONS 66 3.4 VISCOUS FLOW 77 3.5 AIRFOIL
CHARACTERISTICS 85 3.6 CHAPTER SUMMARY 95 3.7 MORE DETAILS 100
REFERENCES 106 PROBLEMS 106 XII CHAPTER 4. WINGS AND AIRPLANES 113 4.1
DESIGN MOTIVATION 113 4.2 WINGS 114 4.3 HIGH-LIFT DEVICES 124 4.4 WHOLE
AIRCRAFT LIFT 128 4.5 WHOLE AIRCRAFT DRAG AND DRAG POLAR 128 4.6
MACH-NUMBER EFFECTS 132 4.7 CHAPTER SUMMARY 143 4.8 MORE DETAILS 150 4.9
WHOLE AIRCRAFT ANALYSIS EXAMPLE 162 REFERENCES 169 PROBLEMS 170 CHAPTER
5. PERFORMANCE 173 5.1 DESIGN MOTIVATION 173 5.2 EQUATIONS OF MOTION 173
5.3 PROPULSION 175 5.4 DRAG CURVES 188 5.5 LIFT-TO-DRAG RATIO 191 5.6
POWER CURVES 192 5.7 CURVE SHIFTS 193 5.8 GLIDES 195 5.9 CLIMBS 198 5.10
RANGE AND ENDURANCE 201 5.11 TAKEOFF AND LANDING 217 5.12 TURNS 224 5.13
V-N DIAGRAMS 231 5.14 ENERGY HEIGHT AND SPECIFIC EXCESS POWER 233 5.15
CHAPTER SUMMARY 238 5.16 MORE DETAILS*MANEUVERABILITY DIAGRAMS AND
CONSTRAINT ANALYSIS 246 5.17 PERFORMANCE ANALYSIS EXAMPLE 253 REFERENCES
260 PROBLEMS 260 CHAPTER 6. STABILITY AND CONTROL 267 6.1 DESIGN
MOTIVATION 267 6.2 LANGUAGE 267 6.3 LONGITUDINAL CONTROL ANALYSIS / 275
6.4 LONGITUDINAL STABILITY 278 6.5 DYNAMIC LONGITUDINAL STABILITY 285
6.6 LATERAL-DIRECTIONAL STABILITY 287 6.7 DYNAMIC LATERAL-DIRECTIONAL
STABILITY 293 6.8 CHAPTER SUMMARY 295 6.9 MORE DETAILS*CALCULATING
STABILITY PARAMETERS 300 6.10 STABILITY AND CONTROL ANALYSIS EXAMPLE:
F-16A AND F-16C 305 REFERENCE 311 PROBLEMS 311 XIII CHAPTER 7.
STRUCTURES 315 7.1 DESIGN MOTIVATION 315 7.2 SOLID MECHANICS 315 7.3
TYPES OF STRESS 321 7.4 LOADS 323 7.5 STRUCTURAL LAYOUT 328 7.6
MATERIALS 331 7.7 COMPONENT SIZING 332 7.8 STRUCTURAL SIZING EXAMPLE 339
7.9 WEIGHT ESTIMATES 340 7.10 FINITE ELEMENT ANALYSIS 340 7.11 CHAPTER
SUMMARY 341 REFERENCES 342 PROBLEMS 342 CHAPTER 8. SIZING 345 8.1 DESIGN
MOTIVATION 345 8.2 INTERNAL LAYOUT 346 8.3 STRUCTURES AND WEIGHT 347 8.4
GEOMETRY CONSTRAINTS 350 8.5 MISSION ANALYSIS 354 8.6 SIZING EQUATION
362 8.7 WEIGHT FRACTION METHOD 364 8.8 WEIGHT AND BALANCE 365 8.9
MISSION ANALYSIS AND SIZING EXAMPLE 367 8.10 AERODYNAMIC 373 8.11 COST
373 8.12 CHAPTER SUMMARY 375 REFERENCES 377 PROBLEMS 378 CHAPTER 9.
PUTTING IT ALL TOGETHER: CONCEPTUAL AIRCRAFT DESIGN . 379 9.1
INTRODUCTION 379 9.2 OVERVIEW OF THE 12 ACTIVITIES 380 9.3 CUSTOMER
FOCUS 381 9.4 DESIGN SYNTHESIS 382 9.5 GEOMETRY MODELING AND ENGINEERING
DRAWING 383 9.6 AERODYNAMIC ANALYSIS 383 9.7 PROPULSION ANALYSIS 386 9.8
CONSTRAINT ANALYSIS 387 9.9 MISSION ANALYSIS 389 9.10 WEIGHT ANALYSIS
390 9.11 SIZING 391 9.12 COST ANALYSIS 392 9.13 OPTIMIZATION 392 9.14
PERFORMANCE REPORTING 393 9.15 PUTTING IT ALL TOGETHER 393 REFERENCES
395 XIV CHAPTER 10. CASE STUDIES AND FUTURE AIRCRAFT DESIGNS 397 10.1
INTRODUCTION 397 10.2 CASE STUDY 1: 1903 WRIGHT FLYER 398 10.3 CASE
STUDY 2: DOUGLAS DC-3 403 10.4 CASE STUDY 3: EVOLUTION OF THE F-16 419
10.5 OPPORTUNITIES IN AIRCRAFT DESIGN 427 10.6 DESIGN THINKING IN OTHER
CONTEXTS 433 REFERENCES 434 APPENDIX A: GLOSSARY 437 APPENDIX B:
SUPPLEMENTAL DATA 449 APPENDIX C: ANSWERS 493 INDEX 503 SUPPORTING
MATERIALS 509 |
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| illustrated | Illustrated |
| index_date | 2024-07-02T16:10:12Z |
| indexdate | 2024-07-09T20:48:47Z |
| institution | BVB |
| isbn | 1563477017 |
| language | English |
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| spelling | Introduction to aeronautics a design perspective 2. ed. Reston, Va. American Inst. of Aeronautics and Astronautics 2004 XXII, 509 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier AIAA education series Avions - Conception et construction Aéronautique Aeronautics Airplanes Design and construction Luftfahrt (DE-588)4036557-8 gnd rswk-swf Luftfahrttechnik (DE-588)4168244-0 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf Aerodynamik (DE-588)4000589-6 s Luftfahrt (DE-588)4036557-8 s 1\p DE-604 Luftfahrttechnik (DE-588)4168244-0 s 2\p DE-604 Brandt, Steven A. Sonstige oth HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015200291&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 | Introduction to aeronautics a design perspective Avions - Conception et construction Aéronautique Aeronautics Airplanes Design and construction Luftfahrt (DE-588)4036557-8 gnd Luftfahrttechnik (DE-588)4168244-0 gnd Aerodynamik (DE-588)4000589-6 gnd |
| subject_GND | (DE-588)4036557-8 (DE-588)4168244-0 (DE-588)4000589-6 |
| title | Introduction to aeronautics a design perspective |
| title_auth | Introduction to aeronautics a design perspective |
| title_exact_search | Introduction to aeronautics a design perspective |
| title_exact_search_txtP | Introduction to aeronautics a design perspective |
| title_full | Introduction to aeronautics a design perspective |
| title_fullStr | Introduction to aeronautics a design perspective |
| title_full_unstemmed | Introduction to aeronautics a design perspective |
| title_short | Introduction to aeronautics |
| title_sort | introduction to aeronautics a design perspective |
| title_sub | a design perspective |
| topic | Avions - Conception et construction Aéronautique Aeronautics Airplanes Design and construction Luftfahrt (DE-588)4036557-8 gnd Luftfahrttechnik (DE-588)4168244-0 gnd Aerodynamik (DE-588)4000589-6 gnd |
| topic_facet | Avions - Conception et construction Aéronautique Aeronautics Airplanes Design and construction Luftfahrt Luftfahrttechnik Aerodynamik |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015200291&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT brandtstevena introductiontoaeronauticsadesignperspective |