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| 001 | 14275182 | ||
| 005 | 20201001163908.0 | ||
| 008 | 060223s2006 enka b 001 0 eng d | ||
| 010 | _a 2006922837 | ||
| 020 | _a0750668172 (hbk.) | ||
| 024 | 3 | _a9780750668170 | |
| 040 |
_aUKM _cUKM _dBAKER _dDLC _erda |
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| 050 | 0 | 0 |
_aTL671.4 _b.F45 2006 |
| 082 | 0 | 4 |
_a629.132 _222 _bF.A.F |
| 100 | 1 |
_aFilippone, Antonio. _926509 _eauthor |
|
| 245 | 1 | 0 |
_aFlight performance of fixed and rotary wing aircraft / _cAntonio Filippone. |
| 250 | _aFirst edition | ||
| 264 |
_aAmsterdam ; _aBoston : _bButterworth-Heinemann, _c2006. |
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| 300 |
_axxvii, 565 pages : _billustrations ; _c26 cm. |
||
| 336 |
_2rdacontent _atext |
||
| 337 |
_2rdamedia _aunmediated |
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| 338 |
_2rdacarrier _avolume |
||
| 440 | 0 |
_aElsevier aerospace engineering series _926510 |
|
| 504 | _aIncludes bibliographical references and index. | ||
| 505 | 0 | _aFront cover -- Title page -- Copyright page -- Table of contents -- Preface -- Acknowledgments -- List of Tables -- Nomenclature: organizations -- Nomenclature: acronyms -- Nomenclature: main symbols -- Nomenclature: Greek symbols -- Nomenclature: subscripts/superscripts -- Supplements to the text -- Part I Fixed-Wing Aircraft Performance -- 1 Introduction -- 1.1 Physical units used -- 1.2 Performance parameters -- 1.3 Performance optimization -- 1.4 Certificate of Airworthiness -- 1.5 Upgrading of aircraft performance -- 1.6 Mission profiles -- 1.6.1 Fighter Aircraft Requirements. 1.6.2 Supersonic Commercial Aircraft Requirements -- Problems -- 2 The aircraft and its environment -- 2.1 General aircraft model -- 2.2 Reference systems -- 2.2.1 Angular Relationships -- 2.3 Forces on the aircraft -- 2.4 Moments of inertia -- 2.5 Flight dynamics equations -- 2.6 The International Standard Atmosphere -- 2.7 Non-standard conditions -- Problems -- 3 Weight performance -- 3.1 The aircraft's weight -- 3.1.1 Wing Loading -- 3.2 Definition of weights -- 3.3 Weight estimation -- 3.4 Weight management -- 3.5 Range/payload diagram -- 3.6 Direct Operating Costs -- Problems. 4 Aerodynamic performance -- 4.1 Aerodynamic forces -- 4.2 Lift equation -- 4.3 Vortex lift -- 4.4 High-lift systems -- 4.5 Drag equation -- 4.5.1 Zero-Lift Drag -- 4.6 Glide ratio -- 4.7 Glide ratio at transonic and supersonic speed -- 4.8 Practical estimation of the drag coefficient -- 4.9 Compressibility effects -- 4.10 Transonic drag rise -- 4.11 Lift and transonic buffet -- 4.12 Aero-thermodynamic heating -- 4.13 Aerodynamic penetration and radius -- 4.14 Aircraft vortex wakes -- 4.15 Aerodynamics and performance -- Problems -- 5 Engine performance -- 5.1 Gas turbine engines. 5.2 Internal combustion engines -- 5.3 Engine flight envelopes -- 5.4 Power and thrust definitions -- 5.5 Generalized engine performance -- 5.6 Fuel flow -- 5.6.1 Aspects of Fuel Consumption -- 5.7 Propulsive efficiency -- 5.8 Thrust characteristics -- 5.9 Propeller characteristics -- 5.9.1 The Axial Momentum Theory -- 5.9.2 The Blade Element Method -- Problems -- 6 Flight envelopes -- 6.1 General definitions -- 6.2 Aircraft speed range -- 6.3 Definition of speeds -- 6.4 Steady state level flight -- 6.5 Speed in level flight -- 6.6 Absolute ceiling of jet aircraft. 6.7 Absolute ceiling of propeller aircraft -- 6.8 Optimal speeds for level flight -- 6.9 General flight envelopes -- 6.10 Limiting factors on flight envelopes -- 6.11 Dash speed of supersonic aircraft -- 6.12 Absolute ceiling of supersonic aircraft -- 6.13 Supersonic acceleration -- 6.13.1 Acceleration at Constant Altitude -- 6.13.2 Other Acceleration Profiles -- Problems -- 7 Take-off and landing -- 7.1 Definition of terminal phases -- 7.2 Conventional take-off -- 7.3 Ground run of jet aircraft -- 7.4 Solutions of the take-off equation -- 7.5 Rotation and initial climb. | |
| 520 | _aCalculation and optimisation of flight performance is required to design or select new aircraft, efficiently operate existing aircraft, and upgrade aircraft. It provides critical data for aircraft certification, accident investigation, fleet management, flight regulations and safety. This book presents an unrivalled range of advanced flight performance models for both transport and military aircraft, including the | ||
| 650 | 0 |
_aAirplanes _xPerformance. _926511 |
|
| 650 | 0 |
_aAerospace engineering. _926512 |
|
| 650 | 0 |
_aFlight engineering. _926513 |
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| 942 |
_cBK _2ddc |
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