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Synthesis of Subsonic Airplane Design, E. Torenbeek


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Цена: 11099.00р.
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Автор: E. Torenbeek
Название:  Synthesis of Subsonic Airplane Design
ISBN: 9789048182732
Издательство: Springer
Классификация: ISBN-10: 9048182735
Обложка/Формат: Paperback
Страницы: 598
Вес: 0.98 кг.
Дата издания: 25.12.2010
Язык: English
Размер: 244 x 170 x 32
Основная тема: Engineering
Подзаголовок: An introduction to the preliminary design of subsonic general aviation and transport aircraft, with emphasis on layout, aerodynamic design, propulsion and performance
Ссылка на Издательство: Link
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Поставляется из: Германии
Описание: 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 students 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 students 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.


Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows

Автор: Lorna Ayton
Название: Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows
ISBN: 3319199587 ISBN-13(EAN): 9783319199580
Издательство: Springer
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Цена: 15672.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: This thesis investigates the sound generated by solid bodies in steady subsonic flows with unsteady perturbations, as is typically used when determining the noise generated by turbulent interactions.

The Theory of Thin Wings in Subsonic Flow

Автор: Serge? Mikha?lovich Belotserkovski?
Название: The Theory of Thin Wings in Subsonic Flow
ISBN: 1489961615 ISBN-13(EAN): 9781489961617
Издательство: Springer
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Цена: 12157.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Flow Modulation and Fluid—Structure Interaction at Airplane Wings

Автор: Josef Ballmann
Название: Flow Modulation and Fluid—Structure Interaction at Airplane Wings
ISBN: 3642536131 ISBN-13(EAN): 9783642536137
Издательство: Springer
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Цена: 16979.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: Besides its scientific value, also the importance of the pro gram for scientific educa- tion becomes evident by looking at the numbers of completed theses, which are up to now about 15 doctoral theses, 40 diploma theses and 70 study theses.

Synthesis of subsonic airplane design

Автор: Torenbeek, Egbert
Название: Synthesis of subsonic airplane design
ISBN: 9400995822 ISBN-13(EAN): 9789400995826
Издательство: Springer
Рейтинг:
Цена: 16979.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: 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.

Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows

Автор: Lorna Ayton
Название: Asymptotic Approximations for the Sound Generated by Aerofoils in Unsteady Subsonic Flows
ISBN: 3319387022 ISBN-13(EAN): 9783319387024
Издательство: Springer
Рейтинг:
Цена: 13059.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: This thesis investigates the sound generated by solid bodies in steady subsonic flows with unsteady perturbations, as is typically used when determining the noise generated by turbulent interactions.

Visualization of Conventional and Combusting Subsonic Jet Instabilities

Автор: Victor V. Kozlov; Genrich R. Grek; Yury A. Litvine
Название: Visualization of Conventional and Combusting Subsonic Jet Instabilities
ISBN: 3319269577 ISBN-13(EAN): 9783319269573
Издательство: Springer
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Цена: 6986.00 р.
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Описание: Based on newinformation obtained on free microjets, this book explains the latest phenomenain flame evolution in the presence of a transverse acoustic field with roundand plane propane microjet combustion.

The Theory of Subsonic Plane Flow

Автор: Woods
Название: The Theory of Subsonic Plane Flow
ISBN: 0521283191 ISBN-13(EAN): 9780521283199
Издательство: Cambridge Academ
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Цена: 8554.00 р.
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Описание: This 1961 book presents a concise and systematic treatment of two-dimensional subsonic, inviscid fluid motion and its aeronautical applications. The text provides an extensive account of mixed boundary-value problems and treats such examples of these problems as occur in ventilated wind-tunnel theory, jet-flap theory and unsteady Hemholtz motions.

Fundamentals of Airplane Flight Mechanics

Автор: David G. Hull
Название: Fundamentals of Airplane Flight Mechanics
ISBN: 3642079873 ISBN-13(EAN): 9783642079870
Издательство: Springer
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Цена: 10480.00 р.
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Описание:

Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This text is concerned with the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane. Algorithms are presented for calculating lift, drag, pitching moment, and stability derivatives. Flight mechanics is a discipline. As such, it has equations of motion, acceptable approximations, and solution techniques for the approximate equations of motion. Once an analytical solution has been obtained, numbers are calculated in order to compare the answer with the assumptions used to derive it and to acquaint students with the sizes of the numbers. A subsonic business jet is used for these calculations.

Air Quality in Airplane Cabins and Similar Enclosed Spaces

Автор: Martin B. Hocking; Diana Hocking
Название: Air Quality in Airplane Cabins and Similar Enclosed Spaces
ISBN: 3642421326 ISBN-13(EAN): 9783642421327
Издательство: Springer
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Цена: 36570.00 р.
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Описание: The issue of aircraft air quality is attracting considerable attention of late, as access to public air travel has expanded exponentially.


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