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Aircraft performance and sizing. Volume II, Applied aerodynamic design /

This book is a concise practical treatise for the student or experienced professional aircraft designer. This volume comprises key applied subjects for performance based aircraft design: systems engineering principles; aircraft mass properties estimation; the aerodynamic design of transonic wings; a...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Takahashi, Timothy, 1966- (Autor)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: New York [New York] (222 East 46th Street, New York, NY 10017) : Momentum Press, 2016.
Colección:Aerospace engineering collection.
Temas:
Acceso en línea:Texto completo

MARC

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100 1 |a Takahashi, Timothy,  |d 1966-  |e author.  |1 https://id.oclc.org/worldcat/entity/E39PCjyWxmgWbDVRrCRcRwrJtC 
245 1 0 |a Aircraft performance and sizing.  |n Volume II,  |p Applied aerodynamic design /  |c Timothy Takahashi. 
246 3 0 |a Applied aerodynamic design 
264 1 |a New York [New York] (222 East 46th Street, New York, NY 10017) :  |b Momentum Press,  |c 2016. 
300 |a 1 online resource (1 PDF (xvii, 250 pages)) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a electronic  |2 isbdmedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a Aerospace engineering collection 
500 |a Title from PDF title page (viewed on March 17, 2016). 
504 |a Includes bibliographical references and index. 
505 0 |a 1. Systems engineering and the design process -- 1.1 The systems engineering vee, a plan for success -- 1.2 Conceptual design -- 1.3 Multidisciplinary trade studies -- 1.4 Model fidelity -- 1.5 Detail design -- 1.6 Risk reduction and mitigation. 
505 8 |a 2. Weight and volume estimation -- 2.1 A self referential problem: how much an aircraft weighs at takeoff is a function of how much it weighs empty -- 2.2 Approaches to aircraft sizing -- 2.3 Empirical methods to estimate empty weight -- 2.4 Modeling and simulation methods to estimate empty weight -- 2.5 Estimating mass moments of inertia. 
505 8 |a 3. Stability and controllability -- 3.1 Aerodynamic database generation -- 3.2 Aerodynamic database presentation -- 3.3 Empirical methods to size the vertical and horizontal tail -- 3.4 Modeling and simulation approach to stability and control -- 3.5 Longitudinal trim -- 3.6 Longitudinal stability -- 3.7 CG placement, horizontal tail, and elevator sizing -- 3.8 Lateral-directional trim -- 3.9 Lateral-directional stability -- 3.10 Lateral-directional control. 
505 8 |a 4. Field performance principles -- 4.1 Takeoff in a nutshell -- 4.2 Simplified statistical method for takeoff -- 4.3 Computing takeoff cue speeds -- 4.4 Modeling and simulation methods for takeoff -- 4.5 Takeoff noise, certification and abatement procedures -- 4.6 Approach and landing in a nutshell -- 4.7 Computing landing cue speeds -- 4.8 Simplified statistical model for landing -- 4.9 Modeling and simulation methods for landing. 
505 8 |a 5. The aerodynamic design of wings -- 5.1 Planform geometry -- 5.2 Three-dimensional flow effects -- 5.3 Transonic flow over two-dimensional airfoils -- 5.4 Selecting an appropriate airfoil for transonic flight -- 5.5 Sweep effects -- 5.6 Nonplanarity -- 5.7 Designing a wing for optimal performance. 
505 8 |a 6. Aircraft sizing and synthesis, putting it all together -- 6.1 Aircraft sizing in a nutshell -- 6.2 Simple sizing using Breguet's equation -- 6.3 Sizing using a multidisciplinary optimization approach -- 6.4 Systems design examples -- 6.5 Afterword -- Index. 
520 3 |a This book is a concise practical treatise for the student or experienced professional aircraft designer. This volume comprises key applied subjects for performance based aircraft design: systems engineering principles; aircraft mass properties estimation; the aerodynamic design of transonic wings; aircraft stability and control; takeoff and landing runway performance. This book may serve as a textbook for an undergraduate aircraft design course or as a reference for the classically trained practicing engineer. 
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590 |a eBooks on EBSCOhost  |b EBSCO eBook Subscription Academic Collection - Worldwide 
650 0 |a Airplanes  |x Design and construction. 
650 0 |a Airplanes  |x Performance. 
650 0 |a Aerodynamics. 
650 6 |a Avions  |x Conception et construction. 
650 6 |a Avions  |x Performances. 
650 6 |a Aérodynamique. 
650 7 |a aerodynamics.  |2 aat 
650 7 |a TECHNOLOGY & ENGINEERING  |x Engineering (General)  |2 bisacsh 
650 7 |a Aerodynamics  |2 fast 
650 7 |a Airplanes  |x Design and construction  |2 fast 
650 7 |a Airplanes  |x Performance  |2 fast 
653 |a Aerodynamics 
653 |a Aircraft Design 
653 |a Aircraft Performance 
653 |a Aircraft Sizing, 
653 |a Drag 
653 |a Lift 
653 |a Aircraft Stability 
653 |a Aircraft Control 
653 |a Aviation 
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