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Introduction to aeronautics : a design perspective /

This text and the accompanying AeroDYNAMIC software are designed for use in teaching basic design methods in an introductory course on aeronautics. Brandt (aeronautics, US Air Force Academy) devotes the first chapter of the text to methods of engineering and aircraft design, then covers basic aerona...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor Corporativo: American Institute of Aeronautics and Astronautics
Otros Autores: Brandt, Steven A., 1953-
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Reston, Va. : American Institute of Aeronautics and Astronautics, ©2004.
Edición:2nd ed.
Colección:AIAA education series.
Temas:
Acceso en línea:Texto completo

MARC

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245 0 0 |a Introduction to aeronautics :  |b a design perspective /  |c Steven A. Brandt [and others]. 
250 |a 2nd ed. 
260 |a Reston, Va. :  |b American Institute of Aeronautics and Astronautics,  |c ©2004. 
300 |a 1 online resource 
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504 |a Includes bibliographical references and index. 
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506 |3 Use copy  |f Restrictions unspecified  |2 star  |5 MiAaHDL 
533 |a Electronic reproduction.  |b [Place of publication not identified] :  |c HathiTrust Digital Library,  |d 2010.  |5 MiAaHDL 
538 |a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.  |u http://purl.oclc.org/DLF/benchrepro0212  |5 MiAaHDL 
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506 |a Access restricted to Ryerson students, faculty and staff.  |5 CaOTR 
505 0 0 |t Design Thinking --  |t Design Method --  |t Design Example --  |t Design and Aeronautics --  |t Brief History of Aircraft Design --  |t Operating Environment --  |t Design Motivation --  |t Characteristics of the Atmosphere --  |t Pressure Measurement --  |t Standard Atmosphere --  |t Common Uses of the Standard Atmosphere --  |t More Details -- Molecular Collisions and Aerodynamics --  |t Aerodynamics and Airfoils --  |t Design Motivation --  |t Basic Aerodynamics --  |t Basic Aerodynamics Applications --  |t Viscous Flow --  |t Airfoil Characteristics --  |t Wings and Airplanes --  |t Design Motivation --  |t Wings --  |t High-Lift Devices --  |t Whole Aircraft Lift --  |t Whole Aircraft Drag and Drag Polar --  |t Mach-Number Effects --  |t Whole Aircraft Analysis Example --  |t Performance --  |t Design Motivation --  |t Equations of Motion --  |t Propulsion --  |t Drag Curves --  |t Lift-to-Drag Ratio --  |t Power Curves --  |t Curve Shifts --  |t Glides --  |t Climbs --  |t Range and Endurance --  |t Takeoff and Landing --  |t Turns --  |t V-n Diagrams --  |t Energy Height and Specific Excess Power --  |t More Details -- Maneuverability Diagrams and Constraint Analysis --  |t Performance Analysis Example --  |t Stability and Control --  |t Design Motivation --  |t Language --  |t Longitudinal Control Analysis --  |t Longitudinal Stability --  |t Dynamic Longitudinal Stability --  |t Lateral-Directional Stability --  |t Dynamic Lateral-Directional Stability --  |t More Details -- Calculating Stability Parameters --  |t Stability and Control Analysis Example: F-16A and F-16C --  |t Structures --  |t Design Motivation --  |t Solid Mechanics --  |t Types of Stress --  |t Loads --  |t Structural Layout --  |t Materials --  |t Component Sizing. 
505 8 0 |t Structural Sizing Example --  |t Weight Estimates --  |t Finite Element Analysis --  |t Sizing --  |t Design Motivation --  |t Internal Layout --  |t Structures and Weight --  |t Geometry Constraints --  |t Mission Analysis --  |t Sizing Equation --  |t Weight Fraction Method --  |t Weight and Balance --  |t Mission Analysis and Sizing Example --  |t AeroDYNAMIC --  |t Cost --  |t Putting It All Together: Conceptual Aircraft Design --  |t Overview of the 12 Activities --  |t Customer Focus --  |t Design Synthesis --  |t Geometry Modeling and Engineering Drawing --  |t Aerodynamic Analysis --  |t Propulsion Analysis --  |t Constraint Analysis --  |t Mission Analysis --  |t Weight Analysis --  |t Sizing --  |t Cost Analysis --  |t Optimization --  |t Performance Reporting --  |t Putting It All Together --  |t Case Studies and Future Aircraft Designs --  |t Case Study 1: 1903 Wright Flyer --  |t Case Study 2: Douglas DC-3 --  |t Case Study 3: Evolution of the F-16 --  |t Opportunities in Aircraft Design --  |t Design Thinking in Other Contexts. 
546 |a English. 
520 |a This text and the accompanying AeroDYNAMIC software are designed for use in teaching basic design methods in an introductory course on aeronautics. Brandt (aeronautics, US Air Force Academy) devotes the first chapter of the text to methods of engineering and aircraft design, then covers basic aeronautical engineering methods used in each step of the design process. Final chapters explain how all of the methods are used in the conceptual aircraft design process and present case studies of the development of three well-known aircraft designs. Previous courses in calculus, classical physics, and engineering mechanics are assumed. Annotation : 2004 Book News, Inc., Portland, OR (booknews.com). 
590 |a ProQuest Ebook Central  |b Ebook Central Academic Complete 
650 0 |a Airplanes  |x Design and construction. 
650 0 |a Aeronautics. 
650 2 |a Aviation 
650 6 |a Avions  |x Conception et construction. 
650 6 |a Aéronautique. 
650 7 |a aviation.  |2 aat 
650 7 |a aeronautics.  |2 aat 
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650 7 |a Airplanes  |x Design and construction  |2 fast 
650 7 |a Aerodynamik  |2 gnd 
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650 7 |a Entwurf  |2 gnd 
650 7 |a Konstruktion  |2 gnd 
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655 7 |a dissertations.  |2 aat 
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655 7 |a Academic theses.  |2 lcgft 
655 7 |a Thèses et écrits académiques.  |2 rvmgf 
700 1 |a Brandt, Steven A.,  |d 1953-  |1 https://id.oclc.org/worldcat/entity/E39PCjyHBvfM4QqDWT8b69Y8bq 
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