EUROSHOCK - Drag Reduction by Passive Shock Control, Egon Stanewsky; Jean Delery; John Fulker; Wolfgang
Автор: Gino Sovran Название: Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles ISBN: 1468484362 ISBN-13(EAN): 9781468484366 Издательство: Springer Рейтинг: Цена: 113190.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: These Proceedings contain the papers and oral discussions presented at the Symposium on AERODYNAMIC DRAG MECHANISMS of Bluff Bodies and Road Vehides held at the General Motors Research Laboratories in Warren, Michigan, on September 27 and 28, 1976.
Автор: Peter Hagedorn; Gottfried Spelsberg-Korspeter Название: Active and Passive Vibration Control of Structures ISBN: 3709119944 ISBN-13(EAN): 9783709119945 Издательство: Springer Рейтинг: Цена: 121890.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Active and Passive Vibration Control of Structures form an issue of very actual interest in many different fields of engineering, for example in the automotive and aerospace industry, in precision engineering (e.g.
Автор: A.K. Belyaev; Michail Z. Kolovsky Название: Nonlinear Dynamics of Active and Passive Systems of Vibration Protection ISBN: 3662222361 ISBN-13(EAN): 9783662222362 Издательство: Springer Рейтинг: Цена: 104480.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: For these reasons, active vibration protection systems, which are actually systems of automatic control with independent power sources, are widely used nowadays. Appearing and developing active systems require that traditional ap- proaches to the analysis and synthesis of vibration protection systems must be revised.
Автор: Egon Stanewsky; J. Delery; John Fulker; Paolo de M Название: Drag Reduction by Shock and Boundary Layer Control ISBN: 3642077625 ISBN-13(EAN): 9783642077623 Издательство: Springer Рейтинг: Цена: 315850.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Concerning aircraft efficiency - relevant to the present research - a reduction in aircraft drag of 10%, a reduction in aircraft fuel consumption of 30%, and a reduction in airframe, engine and system weight of 20% are envisaged.
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