000			03616nam a22002537a 4500
003			ZW-GwMSU
005			20240729134350.0
008			240729b |||||||| |||| 00| 0 eng d
020			_a9780128099988
040			_arda _bEnglish _cMSULIB _erda
050			_aTL671.2 GUD
100	1		_aGudmundsson Snorri _eauthor
245	1	0	_aGeneral aviation aircraft design : applied methods and procedures / _ccreated by Snorri Gudmundsson.
264			_bElsevier, _c2014.
300			_axxi, 1034 pages: _billustrations; _c28 cm
336			_2rdacontent _atext
337			_2rdamedia _aunmediated _bn
338			_2rdacarrier _avolume _bnc
504			_aIncludes bibliography and index
505			_aFront 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
520			_aFind 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.
650		0	_aAirplanes _xDesign and construction
942			_2lcc _cB
999			_c166373 _d166373