Author: Karl Nickel
Publisher: Hodder Education
ISBN:
Category : Business & Economics
Languages : en
Pages : 520
Book Description
Discusses the range of tailless designs, from hanggliders to the US 'Stealth Bomber', and includes a detailed look at particularly significant designs. The authors' own experience in this field allows them to explain and illustrate the topic in a way that appeal to the enthusiast and satisfies the professional aerodynamicist.
Tailless Aircraft in Theory and Practice
Author: Karl Nickel
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Science
Languages : en
Pages : 520
Book Description
The results of a long-term collaboration between a mathematician and a designer, builder, and flier of tailless sailplane models. They provide a comprehensive and practical overview of flying wings, both sailplanes and powered craft. The topics include the aerodynamic principles, stability, control, flight characteristics, design, hanggliders, prejudices and myths, and examples. Accessible to lay readers with some background in flying or aerodynamics. Translated from the 1990 German original. Annotation copyright by Book News, Inc., Portland, OR
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Science
Languages : en
Pages : 520
Book Description
The results of a long-term collaboration between a mathematician and a designer, builder, and flier of tailless sailplane models. They provide a comprehensive and practical overview of flying wings, both sailplanes and powered craft. The topics include the aerodynamic principles, stability, control, flight characteristics, design, hanggliders, prejudices and myths, and examples. Accessible to lay readers with some background in flying or aerodynamics. Translated from the 1990 German original. Annotation copyright by Book News, Inc., Portland, OR
Tailless Aircraft in Theory and Practice
Author: Karl Nickel
Publisher: Hodder Education
ISBN:
Category : Business & Economics
Languages : en
Pages : 520
Book Description
Discusses the range of tailless designs, from hanggliders to the US 'Stealth Bomber', and includes a detailed look at particularly significant designs. The authors' own experience in this field allows them to explain and illustrate the topic in a way that appeal to the enthusiast and satisfies the professional aerodynamicist.
Publisher: Hodder Education
ISBN:
Category : Business & Economics
Languages : en
Pages : 520
Book Description
Discusses the range of tailless designs, from hanggliders to the US 'Stealth Bomber', and includes a detailed look at particularly significant designs. The authors' own experience in this field allows them to explain and illustrate the topic in a way that appeal to the enthusiast and satisfies the professional aerodynamicist.
Theory and Practice of Aircraft Performance
Author: Ajoy Kumar Kundu
Publisher: John Wiley & Sons
ISBN: 1119074185
Category : Technology & Engineering
Languages : en
Pages : 704
Book Description
Textbook introducing the fundamentals of aircraft performance using industry standards and examples: bridging the gap between academia and industry Provides an extensive and detailed treatment of all segments of mission profile and overall aircraft performance Considers operating costs, safety, environmental and related systems issues Includes worked examples relating to current aircraft (Learjet 45, Tucano Turboprop Trainer, Advanced Jet Trainer and Airbus A320 types of aircraft) Suitable as a textbook for aircraft performance courses
Publisher: John Wiley & Sons
ISBN: 1119074185
Category : Technology & Engineering
Languages : en
Pages : 704
Book Description
Textbook introducing the fundamentals of aircraft performance using industry standards and examples: bridging the gap between academia and industry Provides an extensive and detailed treatment of all segments of mission profile and overall aircraft performance Considers operating costs, safety, environmental and related systems issues Includes worked examples relating to current aircraft (Learjet 45, Tucano Turboprop Trainer, Advanced Jet Trainer and Airbus A320 types of aircraft) Suitable as a textbook for aircraft performance courses
Control, Instrumentation and Mechatronics: Theory and Practice
Author: Norhaliza Abdul Wahab
Publisher: Springer Nature
ISBN: 9811939233
Category : Technology & Engineering
Languages : en
Pages : 880
Book Description
This proceeding includes original and peer-reviewed research papers from the 3rd International Conference on Control, Instrumentation and Mechatronics Engineering (CIM2022). The conference is a virtual conference held on 2-3 March 2022. The topics covered latest work and finding in the area of Control Engineering, Mechatronics, Robotics and Automation, Artificial Intelligence, Manufacturing, Sensor, Measurement and Instrumentation. Moreover, the latest applications of instrumentations, control and mechatronics are provided. Therefore, this proceeding is a valuable material for researchers, academicians, university students and engineers.
Publisher: Springer Nature
ISBN: 9811939233
Category : Technology & Engineering
Languages : en
Pages : 880
Book Description
This proceeding includes original and peer-reviewed research papers from the 3rd International Conference on Control, Instrumentation and Mechatronics Engineering (CIM2022). The conference is a virtual conference held on 2-3 March 2022. The topics covered latest work and finding in the area of Control Engineering, Mechatronics, Robotics and Automation, Artificial Intelligence, Manufacturing, Sensor, Measurement and Instrumentation. Moreover, the latest applications of instrumentations, control and mechatronics are provided. Therefore, this proceeding is a valuable material for researchers, academicians, university students and engineers.
An Introduction to Aircraft Performance
Author: Mario Asselin
Publisher: AIAA
ISBN: 9781600860249
Category : Airplanes
Languages : en
Pages : 366
Book Description
Publisher: AIAA
ISBN: 9781600860249
Category : Airplanes
Languages : en
Pages : 366
Book Description
Structural Loads Analysis
Author: Ted L. Lomax
Publisher: AIAA
ISBN: 9781600861185
Category : Airframes
Languages : en
Pages : 306
Book Description
Publisher: AIAA
ISBN: 9781600861185
Category : Airframes
Languages : en
Pages : 306
Book Description
Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations
Author: Bernd Chudoba
Publisher: Springer
ISBN: 3030168565
Category : Technology & Engineering
Languages : en
Pages : 418
Book Description
This book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis. The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific method itself is derived throughout the second half of the book. This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a ‘configuration stability & control’ methodology module for an advanced multi-disciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations?
Publisher: Springer
ISBN: 3030168565
Category : Technology & Engineering
Languages : en
Pages : 418
Book Description
This book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis. The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific method itself is derived throughout the second half of the book. This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a ‘configuration stability & control’ methodology module for an advanced multi-disciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations?
Introduction to Aircraft Flight Mechanics
Author: Thomas R. Yechout
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Aeronautical Engineer's Data Book
Author: Cliff Matthews
Publisher: Elsevier
ISBN: 0080488285
Category : Technology & Engineering
Languages : en
Pages : 282
Book Description
Aeronautical Engineer's Data Bookis an essential handy guide containing useful up to date information regularly needed by the student or practising engineer. Covering all aspects of aircraft, both fixed wing and rotary craft, this pocket book provides quick access to useful aeronautical engineering data and sources of information for further in-depth information. - Quick reference to essential data - Most up to date information available
Publisher: Elsevier
ISBN: 0080488285
Category : Technology & Engineering
Languages : en
Pages : 282
Book Description
Aeronautical Engineer's Data Bookis an essential handy guide containing useful up to date information regularly needed by the student or practising engineer. Covering all aspects of aircraft, both fixed wing and rotary craft, this pocket book provides quick access to useful aeronautical engineering data and sources of information for further in-depth information. - Quick reference to essential data - Most up to date information available
Advanced Dynamics
Author: Shuh-Jing Ying
Publisher: AIAA
ISBN: 9781600860027
Category : Dynamics
Languages : en
Pages : 398
Book Description
Publisher: AIAA
ISBN: 9781600860027
Category : Dynamics
Languages : en
Pages : 398
Book Description