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Author : Jan Roskam
Publisher : DARcorporation
Page : 222 pages
File Size : 54,8 Mb
Release : 1985
Category : Technology & Engineering
ISBN : 188488542X
Author : Jan Roskam
Publisher : DARcorporation
Page : 372 pages
File Size : 40,6 Mb
Release : 1985
Category : Aerospace engineering
ISBN : 1884885543
Author : Jan Roskam
Publisher : Unknown
Page : 228 pages
File Size : 50,6 Mb
Release : 1989
Category : Aerofoils
ISBN : UOM:39015019629859
Author : Jan Roskam
Publisher : DARcorporation
Page : 326 pages
File Size : 55,7 Mb
Release : 1985
Category : Aerospace engineering
ISBN : 1884885438
Author : Egbert Torenbeek
Publisher : John Wiley & Sons
Page : 412 pages
File Size : 51,5 Mb
Release : 2013-05-28
Category : Technology & Engineering
ISBN : 9781118568095
Although 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 : Daniel P. Raymer
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 0 pages
File Size : 54,5 Mb
Release : 2006
Category : Airplanes
ISBN : 1563478293
Winner 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 : Pasquale M. Sforza
Publisher : Elsevier
Page : 623 pages
File Size : 42,7 Mb
Release : 2014-01-31
Category : Technology & Engineering
ISBN : 9780124199774
Commercial Airplane Design Principles is a succinct, focused text covering all the information required at the preliminary stage of aircraft design: initial sizing and weight estimation, fuselage design, engine selection, aerodynamic analysis, stability and control, drag estimation, performance analysis, and economic analysis. The text places emphasis on making informed choices from an array of competing options, and developing the confidence to do so. Shows the use of standard, empirical, and classical methods in support of the design process Explains the preparation of a professional quality design report Provides a sample outline of a design report Can be used in conjunction with Sforza, Manned Spacecraft Design Principles to form a complete course in Aircraft/Spacecraft Design
Author : Snorri Gudmundsson
Publisher : Butterworth-Heinemann
Page : 1048 pages
File Size : 48,6 Mb
Release : 2013-09-03
Category : Technology & Engineering
ISBN : 9780123973290
Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an "equation/derivation/solved example" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design. In most cases, numerical examples involve actual aircraft specs. Concepts are visually depicted by a number of useful black-and-white figures, photos, and graphs (with full-color images included in the eBook only). Broad and deep in coverage, it is intended for practicing engineers, aerospace engineering students, mathematically astute amateur aircraft designers, and anyone interested in aircraft design. Organized by articles and structured in an "equation/derivation/solved example" format for easy access to the content you need Numerical examples involve actual aircraft specs Contains high-interest topics not found in other texts, including sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design Provides a unique safety-oriented design checklist based on industry experience Discusses advantages and disadvantages of using computational tools during the design process Features detailed summaries of design options detailing the pros and cons of each aerodynamic solution Includes three case studies showing applications to business jets, general aviation aircraft, and UAVs Numerous high-quality graphics clearly illustrate the book's concepts (note: images are full-color in eBook only)
Author : Daniel P. Raymer
Publisher : Unknown
Page : 752 pages
File Size : 43,7 Mb
Release : 1989
Category : Technology & Engineering
ISBN : UOM:39015019404253
This textbook for advanced students focuses on industry design practice rather than theoretical definitions. Covers configuration layout, payload considerations, aerodynamics, propulsion, structure and loads, weights, stability, and control, performance, and cost analysis. Annotation copyright Book
Author : Lloyd R. Jenkinson,Jim Marchman
Publisher : Elsevier
Page : 400 pages
File Size : 50,6 Mb
Release : 2003-04-28
Category : Business & Economics
ISBN : 9780080498959
Written with students of aerospace or aeronautical engineering firmly in mind, this is a practical and wide-ranging book that draws together the various theoretical elements of aircraft design - structures, aerodynamics, propulsion, control and others - and guides the reader in applying them in practice. Based on a range of detailed real-life aircraft design projects, including military training, commercial and concept aircraft, the experienced UK and US based authors present engineering students with an essential toolkit and reference to support their own project work. All aircraft projects are unique and it is impossible to provide a template for the work involved in the design process. However, with the knowledge of the steps in the initial design process and of previous experience from similar projects, students will be freer to concentrate on the innovative and analytical aspects of their course project. The authors bring a unique combination of perspectives and experience to this text. It reflects both British and American academic practices in teaching aircraft design. Lloyd Jenkinson has taught aircraft design at both Loughborough and Southampton universities in the UK and Jim Marchman has taught both aircraft and spacecraft design at Virginia Tech in the US. * Demonstrates how basic aircraft design processes can be successfully applied in reality * Case studies allow both student and instructor to examine particular design challenges * Covers commercial and successful student design projects, and includes over 200 high quality illustrations
Author : Jan Roskam
Publisher : Unknown
Page : 438 pages
File Size : 55,5 Mb
Release : 1985
Category : Aerofoils
ISBN : PSU:000031523554
Author : Jan Roskam
Publisher : Unknown
Page : 128 pages
File Size : 53,9 Mb
Release : 1985
Category : Aerospace engineering
ISBN : OCLC:796057450
Author : Jan Roskam
Publisher : DARcorporation
Page : 400 pages
File Size : 55,6 Mb
Release : 1985
Category : Technology & Engineering
ISBN : 1884885551
Author : Egbert Torenbeek
Publisher : Springer Science & Business Media
Page : 630 pages
File Size : 51,8 Mb
Release : 1982-09-30
Category : Technology & Engineering
ISBN : 9024727243
Since the education of aeronautical engineers at Delft University of Technology started in 1940 under tae inspiring leadership of Professor H.J. van der Maas, much emphasis has been placed on the design of aircraft as part of the student's curriculum. Not only is aircraft design an optional subject for thesis work, but every aeronautical student has to carry out a preliminary airplane design in the course of his study. The main purpose of this preliminary design work is to enable the student to synthesize the knowledge ob tained separately in courses on aerodynamics, aircraft performances, stability and con trol, aircraft structures, etc. The student's exercises in preliminary design have been directed through the years by a number of staff members of the Department of Aerospace Engineering in Delft. The author of this book, Mr. E. Torenbeek, has made a large contribution to this part of the study programme for many years. Not only has he acquired vast experience in teaching airplane design at university level, but he has also been deeply involved in design-oriented re search, e.g. developing rational design methods and systematizing design information. I am very pleased that this wealth of experience, methods and data is now presented in this book.
Author : Jan Roskam,Chuan-Tau Edward Lan
Publisher : DARcorporation
Page : 748 pages
File Size : 53,6 Mb
Release : 1997
Category : Science
ISBN : 1884885446
