Gespeichert in:
| Beteilige Person: | |
|---|---|
| Format: | Buch |
| Sprache: | Englisch |
| Veröffentlicht: |
Reston, VA
American Institute of Aeronautics and Astronautics, Inc.
[2018]
|
| Ausgabe: | Sixth edition |
| Schriftenreihe: | AIAA education series
|
| Schlagwörter: | |
| Links: | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=030817056&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| Zusammenfassung: | "Aircraft Design: A Conceptual Approach, Sixth Edition by AIAA Fellow Dr. Daniel P. Raymer provides updates to what has become a standard textbook and reference throughout the world on the subject of aircraft conceptual design. This new edition expands and updates this modern classic including timely topics such as "green aircraft" and electric propulsion, but retains the completeness and readability that have placed it in universities and design offices everywhere. The book covers every topic necessary to the understanding of aircraft design, such as aerodynamics, structures, stability and control, propulsion, etc., with an overview introduction starting from first principles. All are discussed from the point of view of the designer, not the specialist in any given topic area"... |
| Beschreibung: | Includes bibliographical references and index |
| Umfang: | xxx, 1062 Seiten |
| ISBN: | 9781624104909 |
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| 245 | 1 | 0 | |a Aircraft design |b a conceptual approach |c Daniel P. Raymer, Conceptual Research Corporation, Playa del Rey, California |
| 250 | |a Sixth edition | ||
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| 264 | 4 | |c © 2018 | |
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| 490 | 0 | |a AIAA education series | |
| 500 | |a Includes bibliographical references and index | ||
| 520 | |a "Aircraft Design: A Conceptual Approach, Sixth Edition by AIAA Fellow Dr. Daniel P. Raymer provides updates to what has become a standard textbook and reference throughout the world on the subject of aircraft conceptual design. This new edition expands and updates this modern classic including timely topics such as "green aircraft" and electric propulsion, but retains the completeness and readability that have placed it in universities and design offices everywhere. The book covers every topic necessary to the understanding of aircraft design, such as aerodynamics, structures, stability and control, propulsion, etc., with an overview introduction starting from first principles. All are discussed from the point of view of the designer, not the specialist in any given topic area"... | ||
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Datensatz im Suchindex
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|---|---|
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| DE-BY-TUM_location | 03 07 |
| DE-BY-TUM_media_number | 040008759851 040009673747 040008749871 040008759908 040008759873 040008751488 040008759840 040008749860 040008749848 040008759895 040008759884 040008759862 040008759919 040008749882 040008873747 040008749859 |
| _version_ | 1834713153107132416 |
| adam_text | Preface xvii
At, w ■ Awe Cmrayning ijse of Metric Weight Units xix
/AwAAtTilT XX/
Siijjßmüiiiti ttkiteäais xxix
Chapter 1 Design—A Separate Discipline l
1 1 What Is Design? 1
1 2 Design: How Does It Start? 2
1 3 An Airplane Designer: How Can I Become One? 4
1 4 The Book: What Is Here and How It Is Organized 6
Chapter 2 Overview of the Design Process 9
2 1 Requirements 9
2 2 Phases of Aircraft Design 12
2 3 Aircraft Conceptual Design Process 18
2 4 Integrated Product Development and Aircraft Design 23
Chapter 3 Sizing from a Conceptual Sketch 27
3 1 Introduction 27
3 2 Takeoff-Weight Buildup 28
3 3 Empty-Weight Estimation 29
3 4 Fuel-Fraction Estimation 31
3 5 Takeoff-Weight Calculation 42
3 6 Design Example: ASW Aircraft 42
Chapter 4 Airfoil and Wing/ Tail Geometry Selection 53
4 1 Introduction 53
4 2 Airfoil Selection 54
4 3 Wing Geometry 72
XI
ircra esign:
onofcf-i
4 4 Biplane Wings
4 5 Tail Geometry and Arrangement
Chapter 5 Thrust-to-Weight Ratio and Wing Loading
5 1 Introduction
5 2 Thrust-to-Weight Ratio
5 3 Wing Loading
5 4 Selection of Thrust to Weight and Wing Loading
95
97
115
115
116
123
142
Chapter 6 Initial Sizing
6 1 Introduction
6 2 Rubber vs “Fixed-Size” Engines
6 3 Rubber-Engine Sizing
6 4 Fixed-Engine Sizing
6 5 Geometry Sizing
6 6 Control-Surface Sizing
Chapter 7 Configuration Layout and Loft
7 1 Introduction ] 65
7 2 End Products of Configuration Layout 167
7 3 Conic Lofting 175
7 4 Conic Fuselage Development 179
7 5 Flat-Wrap Fuselage Lofting 185
7 6 Circle-to-Square Adapter 188
7 7 Loft Verification via Buttock-Plane Cuts 189
7 8 Wing/Tail Layout and Loft 191
7 9 Wetted-Area Determination 204
7 10 Volume Determination 206
7 11 Use of Computer-Aided Design (CAD)
in Conceptual Design 207
Chapter 8 Special Considerations in Configuration Layout 213
8 1 Introduction 213
8 2 Aerodynamic Considerations 214
8 3 Structural Considerations 223
8 4 Radar Detectability 233
8 5 Infrared Detectability 243
8 6 Visual Detectability 244
8 7 Aural Signature 245
8 8 Vulnerability Considerations 247
8 9 Crashworthiness Considerations 249
8 10 Producibility Considerations 250
8 11 Maintainability Considerations 257
CONTENTS xiii
Chapter 9 Crew Station, Passengers, and Payload 261
9 1 Introduction 261
9 2 Crew Station 262
9 3 Passenger Compartment 266
9 4 Cargo Provisions 267
9 5 Weapons Carriage 269
9 6 Gun Installation 273
Chapter IP impulsion and Fuel System Integration 275
10 1 luiruduaGn 275
10 P s- ::’ Overview and Selection 276
10 0 !: i mtegiation 281
Iß r ■■■■■ Ingme integration 311
10 5 P-■!: 323
10 6 GPropulsion 329
Chapter t i landing Gear and Subsystems 337
11 1 Introduction 337
712 Landing-Gear Arrangements 338
713 Tire Sizing 343
71 4 Shock Absorbers 351
11 5 Castoring-Wheel Geometry 359
11 6 Gear Retraction Geometry 360
11 7 Seaplanes 364
11 8 Subsystems 366
Intermission Step-by-Step Development of a New Design 379
Chapter 12 Aerodynamics 389
12 1 Introduction 389
12 2 Aerodynamic Forces 390
12 3 Aerodynamic Coefficients 396
12 4 Lift 397
12 5 Parasite (Zero-Lift) Drag 416
12 6 Drag Due to Lift (Including Induced Drag) 442
12 7 Computational Fluid Dynamics 452
Chapter 13 Propulsion 463
13 1 Aircraft Thrust—The Big Picture 463
13 2 Jet-Engine Thrust Considerations 466
13 3 Jet-Engine Installed Thrust 469
13 4 Part Power Operation 479
13 5 Piston-Engine Overview 480
iv Aircraft Design: A Conceptual Approach
13 6 Propeller Analysis
13 7 Piston-Prop Thrust Corrections
13 8 Turboprop Performance
Chapter 14 Structures and Loads
14 1 14 2 14 3 Introduction Loads Categories Air Loads 492 494
14 4 Inertial Loads 505
14 5 Powerplant Loads 506
14 6 Landing-Gear Loads 606
14 7 Structures Fundamentals :■!-
14 8 Material Selection 4
14 9 Material Properties “ /
14 10 Structural-Analysis Fundamentals J- /
14 11 Finite Element Structural Analysis 55:
Chapter 15 Weights bS9
15 1 Introduction 559
15 2 Approximate Weight Methods 567
15 3 Aircraft Statistical Weights Method 569
15 4 Additional Considerations in Weights Estimation 579
Chapter 16 Stability, Control, and Handling Qualities 585
16 1 Introduction 585
16 2 Coordinate Systems and Definitions 587
16 3 Longitudinal Static Stability and Control 589
16 4 Lateral-Directional Static Stability and Control 611
16 5 Stick-Free Stability 620
16 6 Effects of Flexibility 620
16 7 Dynamic Stability 622
16 8 Quasi Steady State 627
16 9 Inertia Coupling 629
16 10 Handling Qualities 630
Chapter 17 Performance and Flight Mechanics 637
17 1 Introduction and Equations of Motion 637
17 2 Steady Level Flight 639
17 3 Steady Climbing and Descending Flight 649
17 4 Level Turning Flight 653
17 5 Gliding Flight 657
17 6 Energy-Maneuverability Methods 661
17 7 Operating Envelope 669
CONTENTS xv
17 8 Takeoff Analysis 671
17 9 Landing Analysis 676
17 10 Other Fighter Performance Measures of Merit 679
Chapter 18 Cost Analysis 687
18 1 Introduction 687
18 2 Elements of Life-Cycle Cost 689
18 3 Cost-Estimating Methods 691
18 3 RDT amp;E and Production Costs 692
18 3 C: ;! at ions and Maintenance Costs 699
18 £ C M osones rt Merit (Military) 703
18 ? V :;aC o:M a irline Economics 704
Char- m cm m iMtf Trade Studies 7 09
19, t 1 l: t i J:I 709
19 2 CeiaiicJ SMng Methods 710
19 3 Improved Conceptual Sizing Methods 711
19 4 Classic Optimization—Sizing Matrix and Carpet Plots 717
19 5 Trade Studies 724
Chapter 20 Electric Aircraft 735
20 1 Introduction 735
20 2 Review of Physics amp; Units 738
20 3 Why Spark? 739
20 4 Electric Motor Basics 742
20 5 Power Supply: Batteries 745
20 6 Power Supply: Fuel Cells 749
20 7 Power Supply: Hybricl-Electric 750
20 8 Power Supply: Solar Cells 753
20 9 Power Supply: Beamed Power 754
20 10 Electric Aircraft Run-Time, Range, Loiter, and Climb 755
20 11 Electric Aircraft Initial Sizing
Chapter 21 Vertical Flight—Jet and Prop
21 1 Introduction
21 2 JetVTOL
21 3 Prop VTOL and Helicopter
Chapter 22 Extremes of Flight
22 1 Introduction
22 2 Rockets, Launch Vehicles, and Spacecraft
22 3 Hypersonic Vehicles
22 4 Lighter Than Air
757
763
763
764
783
805
805
806
819
823
vi Aircraft Design: A Conceptual Approach
Chapter 23 Design of Unique Aircraft Concepts 833
23 1 Introduction 833
23 2 Flying Wing, Lifting Fuselage, and Blended Wing Body 834
23 3 Delta and Double-Delta Wing 839
23 4 Forward-Swept Wing 841
23 5 Canard-Pusher 843
23 6 Multi-fuselage 845
23 7 Asymmetric Airplanes 847
23 8 Joined Wing 851
23 9 Some More Innovative Wings 8 •:
23 7 0 Wing-in-Ground-Effect
23 11 Unmanned/Uninhabited Aircraft A C
23 12 Derivative Aircraft Design Chapter 24 Conceptual Design Examples 2
24 1 Introduction 867
24 2 Single-Seat Aerobatic Homebuilt 858
24 3 Lightweight Supercruise Fighter 905
Appendix A Unit Conversion 959
Appendix B Standard Atmosphere 963
Appendixe Airspeed 969
Appendix D Airfoil Data 971
Appendix E Typical Engine Performance Curves 987
E 1 Afterburning Turbofan 987
E 2 High-Bypass Turbofan 991
E 3 Turboprop 993
Appendix f Design Requirements and Specifications 995
Questions 999
|
| any_adam_object | 1 |
| author | Raymer, Daniel P. 1954- |
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| genre | (DE-588)4123623-3 Lehrbuch gnd-content |
| genre_facet | Lehrbuch |
| id | DE-604.BV045431357 |
| illustrated | Not Illustrated |
| indexdate | 2024-12-20T18:27:02Z |
| institution | BVB |
| isbn | 9781624104909 |
| language | English |
| lccn | 018033769 |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-030817056 |
| oclc_num | 1060623923 |
| open_access_boolean | |
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| physical | xxx, 1062 Seiten |
| publishDate | 2018 |
| publishDateSearch | 2018 |
| publishDateSort | 2018 |
| publisher | American Institute of Aeronautics and Astronautics, Inc. |
| record_format | marc |
| series2 | AIAA education series |
| spellingShingle | Raymer, Daniel P. 1954- Aircraft design a conceptual approach Airplanes Design and construction Flugzeug (DE-588)4017672-1 gnd Konstruktion (DE-588)4032231-2 gnd Flugzeugbau (DE-588)4154782-2 gnd Entwurf (DE-588)4121208-3 gnd |
| subject_GND | (DE-588)4017672-1 (DE-588)4032231-2 (DE-588)4154782-2 (DE-588)4121208-3 (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_full | Aircraft design a conceptual approach Daniel P. Raymer, Conceptual Research Corporation, Playa del Rey, California |
| title_fullStr | Aircraft design a conceptual approach Daniel P. Raymer, Conceptual Research Corporation, Playa del Rey, California |
| title_full_unstemmed | Aircraft design a conceptual approach Daniel P. Raymer, Conceptual Research Corporation, Playa del Rey, California |
| title_short | Aircraft design |
| title_sort | aircraft design a conceptual approach |
| title_sub | a conceptual approach |
| topic | Airplanes Design and construction Flugzeug (DE-588)4017672-1 gnd Konstruktion (DE-588)4032231-2 gnd Flugzeugbau (DE-588)4154782-2 gnd Entwurf (DE-588)4121208-3 gnd |
| topic_facet | Airplanes Design and construction Flugzeug Konstruktion Flugzeugbau Entwurf Lehrbuch |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=030817056&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT raymerdanielp aircraftdesignaconceptualapproach |
Inhaltsverzeichnis
Paper/Kapitel scannen lassen
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Teilbibliothek Chemie, Lehrbuchsammlung
Teilbibliothek Maschinenwesen
| Signatur: | 0704 VER 600 2007 A 1984(6) |
|---|---|
| Exemplar 1 | Nicht ausleihbar Am Standort |