General aviation aircraft design: applied methods and procedures
Saved in:
| Main Author: | |
|---|---|
| Format: | Electronic eBook |
| Language: | English |
| Published: |
Oxford, UK
Butterworth-Heinemann
[2014]
|
| Edition: | First edition |
| Subjects: | |
| Online Access: | FAW01 FAW02 |
| Item Description: | Online resource; title from PDF title page (ebrary, viewed September 17, 2013) |
| Physical Description: | 1 online resource (1048 pages) illustrations |
| ISBN: | 9780123973290 0123973295 0123973082 9780123973085 |
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| 505 | 8 | |a Front Cover; Dedication; GENERAL AVIATION AIRCRAFT DESIGN: APPLIED METHODS AND PROCEDURES; Copyright; Contents; Chapter 1 -- The Aircraft Design Process; 1.1 INTRODUCTION; 1.2 GENERAL PROCESS OF AIRCRAFT DESIGN; 1.3 AIRCRAFT DESIGN ALGORITHM; 1.4 ELEMENTS OF PROJECT ENGINEERING; 1.5 PRESENTING THE DESIGN PROJECT; VARIABLES; References; Chapter 2 -- Aircraft Cost Analysis; 2.1 INTRODUCTION; 2.2 ESTIMATING PROJECT DEVELOPMENT COSTS; 2.3 ESTIMATING AIRCRAFT OPERATIONAL COSTS; EXERCISES; VARIABLES; References; Chapter 3 -- Initial Sizing; 3.1 INTRODUCTION; 3.2 CONSTRAINT ANALYSIS. | |
| 505 | 8 | |a 3.3 INTRODUCTION TO TRADE STUDIESEXERCISES; VARIABLES; Chapter 4 -- Aircraft Conceptual Layout; 4.1 INTRODUCTION; 4.2 THE FUNDAMENTALS OF THE CONFIGURATION LAYOUT; VARIABLES; References; Chapter 5 -- Aircraft Structural Layout; 5.1 INTRODUCTION; 5.2 AIRCRAFT FABRICATION AND MATERIALS; 5.3 AIRFRAME STRUCTURAL LAYOUT; VARIABLES; References; Chapter 6 -- Aircraft Weight Analysis; 6.1 INTRODUCTION; 6.2 INITIAL WEIGHT ANALYSIS METHODS; 6.3 DETAILED WEIGHT ANALYSIS METHODS; 6.4 STATISTICAL WEIGHT ESTIMATION METHODS; 6.5 DIRECT WEIGHT ESTIMATION METHODS; 6.6 INERTIA PROPERTIES; EXERCISES; VARIABLES. | |
| 505 | 8 | |a 9.6 WING STALL CHARACTERISTICS9.7 NUMERICAL ANALYSIS OF THE WING; EXERCISES; VARIABLES; References; Chapter 10 -- The Anatomy of Lift Enhancement; 10.1 INTRODUCTION; 10.2 LEADING-EDGE HIGH-LIFT DEVICES; 10.3 TRAILING EDGE HIGH-LIFT DEVICES; 10.4 EFFECT OF DEPLOYING HIGH-LIFT DEVICES ON WINGS; 10.5 WINGTIP DESIGN; VARIABLES; References; Chapter 11 -- The Anatomy of the Tail; 11.1 INTRODUCTION; 11.2 FUNDAMENTALS OF STATIC STABILITY AND CONTROL; 11.3 ON THE PROS AND CONS OF TAIL CONFIGURATIONS; 11.4 THE GEOMETRY OF THE TAIL; 11.5 INITIAL TAIL SIZING METHODS; EXERCISES; VARIABLES; References | |
| 505 | 8 | |a Chapter 12 -- The Anatomy of the Fuselage12.1 INTRODUCTION; 12.2 FUNDAMENTALS OF FUSELAGE SHAPES; 12.3 SIZING THE FUSELAGE; 12.4 ESTIMATING THE GEOMETRIC PROPERTIES OF THE FUSELAGE; 12.5 ADDITIONAL INFORMATION; VARIABLES; References; Chapter 13 -- The Anatomy of the Landing Gear; 13.1 INTRODUCTION; 13.2 TIRES, WHEELS, AND BRAKES; 13.3 GEOMETRIC LAYOUT OF THE LANDING GEAR; VARIABLES; References; Chapter 14 -- The Anatomy of the Propeller; 14.1 INTRODUCTION; 14.2 PROPELLER EFFECTS; 14.3 PROPERTIES AND SELECTION OF THE PROPELLER; 14.4 DETERMINATION OF PROPELLER THRUST. | |
| 505 | 8 | |a Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an ""equation/derivation/solved example"" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, siz | |
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Record in the Search Index
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| any_adam_object | |
| author | Gudmundsson, Snorri |
| author_facet | Gudmundsson, Snorri |
| author_role | aut |
| author_sort | Gudmundsson, Snorri |
| author_variant | s g sg |
| building | Verbundindex |
| bvnumber | BV043957931 |
| collection | ZDB-4-EBA ZDB-4-ENC |
| contents | Front Cover; Dedication; GENERAL AVIATION AIRCRAFT DESIGN: APPLIED METHODS AND PROCEDURES; Copyright; Contents; Chapter 1 -- The Aircraft Design Process; 1.1 INTRODUCTION; 1.2 GENERAL PROCESS OF AIRCRAFT DESIGN; 1.3 AIRCRAFT DESIGN ALGORITHM; 1.4 ELEMENTS OF PROJECT ENGINEERING; 1.5 PRESENTING THE DESIGN PROJECT; VARIABLES; References; Chapter 2 -- Aircraft Cost Analysis; 2.1 INTRODUCTION; 2.2 ESTIMATING PROJECT DEVELOPMENT COSTS; 2.3 ESTIMATING AIRCRAFT OPERATIONAL COSTS; EXERCISES; VARIABLES; References; Chapter 3 -- Initial Sizing; 3.1 INTRODUCTION; 3.2 CONSTRAINT ANALYSIS. 3.3 INTRODUCTION TO TRADE STUDIESEXERCISES; VARIABLES; Chapter 4 -- Aircraft Conceptual Layout; 4.1 INTRODUCTION; 4.2 THE FUNDAMENTALS OF THE CONFIGURATION LAYOUT; VARIABLES; References; Chapter 5 -- Aircraft Structural Layout; 5.1 INTRODUCTION; 5.2 AIRCRAFT FABRICATION AND MATERIALS; 5.3 AIRFRAME STRUCTURAL LAYOUT; VARIABLES; References; Chapter 6 -- Aircraft Weight Analysis; 6.1 INTRODUCTION; 6.2 INITIAL WEIGHT ANALYSIS METHODS; 6.3 DETAILED WEIGHT ANALYSIS METHODS; 6.4 STATISTICAL WEIGHT ESTIMATION METHODS; 6.5 DIRECT WEIGHT ESTIMATION METHODS; 6.6 INERTIA PROPERTIES; EXERCISES; VARIABLES. 9.6 WING STALL CHARACTERISTICS9.7 NUMERICAL ANALYSIS OF THE WING; EXERCISES; VARIABLES; References; Chapter 10 -- The Anatomy of Lift Enhancement; 10.1 INTRODUCTION; 10.2 LEADING-EDGE HIGH-LIFT DEVICES; 10.3 TRAILING EDGE HIGH-LIFT DEVICES; 10.4 EFFECT OF DEPLOYING HIGH-LIFT DEVICES ON WINGS; 10.5 WINGTIP DESIGN; VARIABLES; References; Chapter 11 -- The Anatomy of the Tail; 11.1 INTRODUCTION; 11.2 FUNDAMENTALS OF STATIC STABILITY AND CONTROL; 11.3 ON THE PROS AND CONS OF TAIL CONFIGURATIONS; 11.4 THE GEOMETRY OF THE TAIL; 11.5 INITIAL TAIL SIZING METHODS; EXERCISES; VARIABLES; References Chapter 12 -- The Anatomy of the Fuselage12.1 INTRODUCTION; 12.2 FUNDAMENTALS OF FUSELAGE SHAPES; 12.3 SIZING THE FUSELAGE; 12.4 ESTIMATING THE GEOMETRIC PROPERTIES OF THE FUSELAGE; 12.5 ADDITIONAL INFORMATION; VARIABLES; References; Chapter 13 -- The Anatomy of the Landing Gear; 13.1 INTRODUCTION; 13.2 TIRES, WHEELS, AND BRAKES; 13.3 GEOMETRIC LAYOUT OF THE LANDING GEAR; VARIABLES; References; Chapter 14 -- The Anatomy of the Propeller; 14.1 INTRODUCTION; 14.2 PROPELLER EFFECTS; 14.3 PROPERTIES AND SELECTION OF THE PROPELLER; 14.4 DETERMINATION OF PROPELLER THRUST. Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an ""equation/derivation/solved example"" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, siz |
| ctrlnum | (ZDB-4-EBA)ocn861528482 (ZDB-4-ENC)ocn861528482 (OCoLC)861528482 (DE-599)BVBBV043957931 |
| dewey-full | 629.13334 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.13334 |
| dewey-search | 629.13334 |
| dewey-sort | 3629.13334 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| edition | First edition |
| format | Electronic eBook |
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| id | DE-604.BV043957931 |
| illustrated | Illustrated |
| indexdate | 2024-07-10T07:39:43Z |
| institution | BVB |
| isbn | 9780123973290 0123973295 0123973082 9780123973085 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029366634 |
| oclc_num | 861528482 |
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| physical | 1 online resource (1048 pages) illustrations |
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| publishDate | 2014 |
| publishDateSearch | 2014 |
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| publisher | Butterworth-Heinemann |
| record_format | marc |
| spelling | Gudmundsson, Snorri Verfasser aut General aviation aircraft design applied methods and procedures Snorri Gudmundsson First edition Oxford, UK Butterworth-Heinemann [2014] © 2014 1 online resource (1048 pages) illustrations txt rdacontent c rdamedia cr rdacarrier Online resource; title from PDF title page (ebrary, viewed September 17, 2013) Front Cover; Dedication; GENERAL AVIATION AIRCRAFT DESIGN: APPLIED METHODS AND PROCEDURES; Copyright; Contents; Chapter 1 -- The Aircraft Design Process; 1.1 INTRODUCTION; 1.2 GENERAL PROCESS OF AIRCRAFT DESIGN; 1.3 AIRCRAFT DESIGN ALGORITHM; 1.4 ELEMENTS OF PROJECT ENGINEERING; 1.5 PRESENTING THE DESIGN PROJECT; VARIABLES; References; Chapter 2 -- Aircraft Cost Analysis; 2.1 INTRODUCTION; 2.2 ESTIMATING PROJECT DEVELOPMENT COSTS; 2.3 ESTIMATING AIRCRAFT OPERATIONAL COSTS; EXERCISES; VARIABLES; References; Chapter 3 -- Initial Sizing; 3.1 INTRODUCTION; 3.2 CONSTRAINT ANALYSIS. 3.3 INTRODUCTION TO TRADE STUDIESEXERCISES; VARIABLES; Chapter 4 -- Aircraft Conceptual Layout; 4.1 INTRODUCTION; 4.2 THE FUNDAMENTALS OF THE CONFIGURATION LAYOUT; VARIABLES; References; Chapter 5 -- Aircraft Structural Layout; 5.1 INTRODUCTION; 5.2 AIRCRAFT FABRICATION AND MATERIALS; 5.3 AIRFRAME STRUCTURAL LAYOUT; VARIABLES; References; Chapter 6 -- Aircraft Weight Analysis; 6.1 INTRODUCTION; 6.2 INITIAL WEIGHT ANALYSIS METHODS; 6.3 DETAILED WEIGHT ANALYSIS METHODS; 6.4 STATISTICAL WEIGHT ESTIMATION METHODS; 6.5 DIRECT WEIGHT ESTIMATION METHODS; 6.6 INERTIA PROPERTIES; EXERCISES; VARIABLES. 9.6 WING STALL CHARACTERISTICS9.7 NUMERICAL ANALYSIS OF THE WING; EXERCISES; VARIABLES; References; Chapter 10 -- The Anatomy of Lift Enhancement; 10.1 INTRODUCTION; 10.2 LEADING-EDGE HIGH-LIFT DEVICES; 10.3 TRAILING EDGE HIGH-LIFT DEVICES; 10.4 EFFECT OF DEPLOYING HIGH-LIFT DEVICES ON WINGS; 10.5 WINGTIP DESIGN; VARIABLES; References; Chapter 11 -- The Anatomy of the Tail; 11.1 INTRODUCTION; 11.2 FUNDAMENTALS OF STATIC STABILITY AND CONTROL; 11.3 ON THE PROS AND CONS OF TAIL CONFIGURATIONS; 11.4 THE GEOMETRY OF THE TAIL; 11.5 INITIAL TAIL SIZING METHODS; EXERCISES; VARIABLES; References Chapter 12 -- The Anatomy of the Fuselage12.1 INTRODUCTION; 12.2 FUNDAMENTALS OF FUSELAGE SHAPES; 12.3 SIZING THE FUSELAGE; 12.4 ESTIMATING THE GEOMETRIC PROPERTIES OF THE FUSELAGE; 12.5 ADDITIONAL INFORMATION; VARIABLES; References; Chapter 13 -- The Anatomy of the Landing Gear; 13.1 INTRODUCTION; 13.2 TIRES, WHEELS, AND BRAKES; 13.3 GEOMETRIC LAYOUT OF THE LANDING GEAR; VARIABLES; References; Chapter 14 -- The Anatomy of the Propeller; 14.1 INTRODUCTION; 14.2 PROPELLER EFFECTS; 14.3 PROPERTIES AND SELECTION OF THE PROPELLER; 14.4 DETERMINATION OF PROPELLER THRUST. Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an ""equation/derivation/solved example"" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, siz TECHNOLOGY & ENGINEERING / Engineering (General) bisacsh Airplanes / Design and construction fast Airplanes Design and construction Flugzeug (DE-588)4017672-1 gnd rswk-swf Flugzeugbau (DE-588)4154782-2 gnd rswk-swf Konstruieren (DE-588)4139312-0 gnd rswk-swf 1\p (DE-588)4123623-3 Lehrbuch gnd-content Flugzeug (DE-588)4017672-1 s Flugzeugbau (DE-588)4154782-2 s Konstruieren (DE-588)4139312-0 s 2\p DE-604 Erscheint auch als Druck-Ausgabe Gudmundsson, Snorri General Aviation Aircraft Design : Applied Methods and Procedures 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 | Gudmundsson, Snorri General aviation aircraft design applied methods and procedures Front Cover; Dedication; GENERAL AVIATION AIRCRAFT DESIGN: APPLIED METHODS AND PROCEDURES; Copyright; Contents; Chapter 1 -- The Aircraft Design Process; 1.1 INTRODUCTION; 1.2 GENERAL PROCESS OF AIRCRAFT DESIGN; 1.3 AIRCRAFT DESIGN ALGORITHM; 1.4 ELEMENTS OF PROJECT ENGINEERING; 1.5 PRESENTING THE DESIGN PROJECT; VARIABLES; References; Chapter 2 -- Aircraft Cost Analysis; 2.1 INTRODUCTION; 2.2 ESTIMATING PROJECT DEVELOPMENT COSTS; 2.3 ESTIMATING AIRCRAFT OPERATIONAL COSTS; EXERCISES; VARIABLES; References; Chapter 3 -- Initial Sizing; 3.1 INTRODUCTION; 3.2 CONSTRAINT ANALYSIS. 3.3 INTRODUCTION TO TRADE STUDIESEXERCISES; VARIABLES; Chapter 4 -- Aircraft Conceptual Layout; 4.1 INTRODUCTION; 4.2 THE FUNDAMENTALS OF THE CONFIGURATION LAYOUT; VARIABLES; References; Chapter 5 -- Aircraft Structural Layout; 5.1 INTRODUCTION; 5.2 AIRCRAFT FABRICATION AND MATERIALS; 5.3 AIRFRAME STRUCTURAL LAYOUT; VARIABLES; References; Chapter 6 -- Aircraft Weight Analysis; 6.1 INTRODUCTION; 6.2 INITIAL WEIGHT ANALYSIS METHODS; 6.3 DETAILED WEIGHT ANALYSIS METHODS; 6.4 STATISTICAL WEIGHT ESTIMATION METHODS; 6.5 DIRECT WEIGHT ESTIMATION METHODS; 6.6 INERTIA PROPERTIES; EXERCISES; VARIABLES. 9.6 WING STALL CHARACTERISTICS9.7 NUMERICAL ANALYSIS OF THE WING; EXERCISES; VARIABLES; References; Chapter 10 -- The Anatomy of Lift Enhancement; 10.1 INTRODUCTION; 10.2 LEADING-EDGE HIGH-LIFT DEVICES; 10.3 TRAILING EDGE HIGH-LIFT DEVICES; 10.4 EFFECT OF DEPLOYING HIGH-LIFT DEVICES ON WINGS; 10.5 WINGTIP DESIGN; VARIABLES; References; Chapter 11 -- The Anatomy of the Tail; 11.1 INTRODUCTION; 11.2 FUNDAMENTALS OF STATIC STABILITY AND CONTROL; 11.3 ON THE PROS AND CONS OF TAIL CONFIGURATIONS; 11.4 THE GEOMETRY OF THE TAIL; 11.5 INITIAL TAIL SIZING METHODS; EXERCISES; VARIABLES; References Chapter 12 -- The Anatomy of the Fuselage12.1 INTRODUCTION; 12.2 FUNDAMENTALS OF FUSELAGE SHAPES; 12.3 SIZING THE FUSELAGE; 12.4 ESTIMATING THE GEOMETRIC PROPERTIES OF THE FUSELAGE; 12.5 ADDITIONAL INFORMATION; VARIABLES; References; Chapter 13 -- The Anatomy of the Landing Gear; 13.1 INTRODUCTION; 13.2 TIRES, WHEELS, AND BRAKES; 13.3 GEOMETRIC LAYOUT OF THE LANDING GEAR; VARIABLES; References; Chapter 14 -- The Anatomy of the Propeller; 14.1 INTRODUCTION; 14.2 PROPELLER EFFECTS; 14.3 PROPERTIES AND SELECTION OF THE PROPELLER; 14.4 DETERMINATION OF PROPELLER THRUST. Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an ""equation/derivation/solved example"" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, siz TECHNOLOGY & ENGINEERING / Engineering (General) bisacsh Airplanes / Design and construction fast Airplanes Design and construction Flugzeug (DE-588)4017672-1 gnd Flugzeugbau (DE-588)4154782-2 gnd Konstruieren (DE-588)4139312-0 gnd |
| subject_GND | (DE-588)4017672-1 (DE-588)4154782-2 (DE-588)4139312-0 (DE-588)4123623-3 |
| title | General aviation aircraft design applied methods and procedures |
| title_auth | General aviation aircraft design applied methods and procedures |
| title_exact_search | General aviation aircraft design applied methods and procedures |
| title_full | General aviation aircraft design applied methods and procedures Snorri Gudmundsson |
| title_fullStr | General aviation aircraft design applied methods and procedures Snorri Gudmundsson |
| title_full_unstemmed | General aviation aircraft design applied methods and procedures Snorri Gudmundsson |
| title_short | General aviation aircraft design |
| title_sort | general aviation aircraft design applied methods and procedures |
| title_sub | applied methods and procedures |
| topic | TECHNOLOGY & ENGINEERING / Engineering (General) bisacsh Airplanes / Design and construction fast Airplanes Design and construction Flugzeug (DE-588)4017672-1 gnd Flugzeugbau (DE-588)4154782-2 gnd Konstruieren (DE-588)4139312-0 gnd |
| topic_facet | TECHNOLOGY & ENGINEERING / Engineering (General) Airplanes / Design and construction Airplanes Design and construction Flugzeug Flugzeugbau Konstruieren Lehrbuch |
| work_keys_str_mv | AT gudmundssonsnorri generalaviationaircraftdesignappliedmethodsandprocedures |