Advances in Hypersonics, BALLMANN; BERTIN; PERIAUX

Автор: Bertin; Ballmann; Periaux
Название: Advances in Hypersonics
ISBN: 1461267307 ISBN-13(EAN): 9781461267300
Издательство: Springer
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Автор: T.K.S. Murthy
Название: Computational Methods in Hypersonic Aerodynamics
ISBN: 0792316738 ISBN-13(EAN): 9780792316732
Издательство: Springer
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Описание: Contains chapters on computational methods in hypersonic aerodynamics. This book includes the effects of viscosity on the physical and chemical processes of high-temperature nonequilibrium flow at very high speeds, such as vibrational excitation, dissociation and recombination, and ionization and radiation.

Автор: BERTIN; GLOWINSKI; PERIAUX
Название: Hypersonics
ISBN: 146849189X ISBN-13(EAN): 9781468491890
Издательство: Springer
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Описание: Configurations that have a relatively high ballistic coefficient (such as slender reentry vehicles) and reenter the atmosphere at relatively high angles of attack experience severe heating rates and high dynamic pressures, but only for a short period of time.

Автор: Hannes Stephan Griebel
Название: Reaching High Altitudes on Mars With an Inflatable Hypersonic Drag Balloon
ISBN: 3834814253 ISBN-13(EAN): 9783834814258
Издательство: Springer
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Описание: Tbe main purpose of this work was to find a way of placing a meaningful scientific payload within the upper atmosphere of Mars such that certain scientific measurements become possible. So the altitude range covered and the possible dweIl time are relevant design drivers and will be explored in greater detail within this thesis. Either concept of flying on Mars, however, be it heavier or lighter than air (read: heavier or lighter than carbon dioxide) is restricted to altitodes weil below 10 km. Since any sustained light at that altitode or higher in such a thin atmosphere is teehnically impractical, so is ascending to that altitode with - sounding rocket. Therefore - team of scientists from several research institutes around Europe fonned a scientific committec. Together with engineers and scientists from tbe Mars Society Germany and tbe University ofthe Federal Armed Forces of Germany in Munich (UBW) the committee drafted a reference scientific mission scenario 1] to: find ways to da exactly that: providing an instrument suite with access to a large altitu. de range and. meaningful dwell time (see 10. 3. 1 starting onp. ge 208). Tbc most practical approach was found in an inflatable entry vehicle that can provide the largest and lightest possible configuration. Since 00 such attempts have yet been m. ade, the work described herein focuses mostly on the mathematical thcory and the technical peculiarities of such a system, but also treats mission design and testing aspects. 1.