Scientific and Technical Aerospace Reports
Author:
Publisher:
Published: 1995
Total Pages: 692
ISBN-13:
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Author:
Publisher:
Published: 1995
Total Pages: 692
ISBN-13:
DOWNLOAD EBOOKAuthor: Egbert Torenbeek
Publisher: John Wiley & Sons
Published: 2013-07-29
Total Pages: 452
ISBN-13: 1118568117
DOWNLOAD EBOOKAlthough the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered. The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to “what if” questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimization Provides an overview of advanced technologies for propulsion and reducing aerodynamic drag Offers insight into the derivation of design sensitivity information Emphasizes design based on first principles Considers pros and cons of innovative configurations Reconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts.
Author: Ramesh K. Agarwal
Publisher: BoD – Books on Demand
Published: 2016-09-08
Total Pages: 206
ISBN-13: 9535124811
DOWNLOAD EBOOKThe book describes the recent progress in some engine technologies and active flow control and morphing technologies and in topics related to aeroacoustics and aircraft controllers. Both the researchers and students should find the material useful in their work.
Author:
Publisher:
Published: 1995
Total Pages: 1166
ISBN-13:
DOWNLOAD EBOOKAuthor: Jochen Wild
Publisher: CRC Press
Published: 2022-02-03
Total Pages: 372
ISBN-13: 1000532623
DOWNLOAD EBOOKThis book presents a detailed look at high-lift aerodynamics, which deals with the aerodynamic behavior of lift augmentation means from various approaches. After an introductory chapter, the book discusses the physical limits of lift generation, giving the lift generation potential. It then explains what is needed for an aircraft to fly safely by analyzing the high-lift-related requirements for certifying an aircraft. Aircraft needs are also analyzed to improve performance during takeoff, approach, and landing. The book discusses in detail the applied means to increase the lift coefficient by either passive and active high-lift systems. It includes slotless and slotted high-lift flaps, active and passive vortex generating devices, boundary and circulation control, and powered lift. Describing methods that are used to evaluate and design high-lift systems in an aerodynamic sense, the book briefly covers numerical as well as experimental simulation methods. It also includes a chapter on the aerodynamic design of high-lift systems. FEATURES Provides an understanding of the physics of flight during takeoff and landing from aerodynamics to flight performance and from simulation to design Discusses the physical limits of lift generation, giving the lift generation potential Concentrates on the specifics of high-lift aerodynamics to provide a first insight Analyzes aircraft needs to improve performance during takeoff, approach, and landing Focuses on civil transport aircraft applications but also includes the associated physics that apply to all aircraft This book is intended for graduate students in aerospace programs studying advanced aerodynamics and aircraft design. It also serves as a professional reference for practicing aerospace and mechanical engineers who are working on aircraft design issues related to takeoff and landing.
Author: National Research Council (U.S.). Committee on Aeronautical Technologies
Publisher:
Published: 1992
Total Pages: 21
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1967
Total Pages: 412
ISBN-13:
DOWNLOAD EBOOKAuthor: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
Published: 199?
Total Pages: 710
ISBN-13:
DOWNLOAD EBOOKAuthor: Shriram Hegde
Publisher: Springer Nature
Published: 2022-11-25
Total Pages: 288
ISBN-13: 9811941408
DOWNLOAD EBOOKThe book presents select proceedings of the International Conference on Mechanical Engineering (INCOME 2021). It includes the topics related to design and functional requirements of components used in mechanical systems. The contents covered include concept design, detailed design, structural design, mechanics, static and dynamic systems. The book also discusses various methods of software aided design and analysis. Given the contents, the book will be a valuable reference for beginners, researchers, and professionals working in various domains of mechanical engineering.