Aircraft Journal
Author:
Publisher:
Published: 1920
Total Pages: 364
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author:
Publisher:
Published: 1921
Total Pages: 520
ISBN-13:
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Publisher:
Published: 1921
Total Pages: 764
ISBN-13:
DOWNLOAD EBOOKAuthor: Daniel P. Raymer
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Published: 2006
Total Pages: 0
ISBN-13: 9781563478291
DOWNLOAD EBOOKWinner of the Summerfield Book Award Winner of the Aviation-Space Writers Association Award of Excellence. --Over 30,000 copies sold, consistently the top-selling AIAA textbook title This highly regarded textbook presents the entire process of aircraft conceptual designfrom requirements definition to initial sizing, configuration layout, analysis, sizing, and trade studiesin the same manner seen in industry aircraft design groups. Interesting and easy to read, the book has more than 800 pages of design methods, illustrations, tips, explanations, and equations, and extensive appendices with key data essential to design. It is the required design text at numerous universities around the world, and is a favorite of practicing design engineers.
Author: United States. Civil Aeronautics Administration
Publisher:
Published: 1952
Total Pages: 72
ISBN-13:
DOWNLOAD EBOOKAuthor: Egbert Torenbeek
Publisher: John Wiley & Sons
Published: 2013-05-28
Total Pages: 412
ISBN-13: 1118568095
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: Robert E. Ball
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Published: 2003
Total Pages: 952
ISBN-13:
DOWNLOAD EBOOKFrom infant car seats to the design of aircraft cargo bay structures that can withstand bomb blasts, the government is taking the lead in survivability standards. The extensively illustrated new edition of this book presents the fundamentals of the aircraft combat survivability design discipline as defined by the DoD military standards and acquisition processes.