Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware 68 pp. Englisch. N° de réf. du vendeur 9786207460793
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Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The ejector mode concept in rocket-based combined cycles presents an opportunity to derive thrust from atmospheric air, thereby diminishing fuel consumption and reducing overall rocket launch costs. This project concentrates on crafting a three-dimensional rocket nozzle featuring the ejector effect. The design involves a diverging section passing through a non-axisymmetric gate or clover on the outer perimeter, creating a void for air intake into the center of an annular rocket exhaust stream. The primary objective is to pinpoint the optimal design among three configurations with varying clover numbers (3, 4, and 5). Flow analyses, utilizing numerical simulations and a predefined Mach number distribution, were conducted, incorporating viscous simulations with the k- turbulence model. Results reveal that the nozzle with 4 clovers outperforms those with 3 or 5 clovers, aligning closely with predefined outlet Mach numbers and demonstrating effectiveness. N° de réf. du vendeur 9786207460793
Quantité disponible : 1 disponible(s)
Vendeur : moluna, Greven, Allemagne
Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. The ejector mode concept in rocket-based combined cycles presents an opportunity to derive thrust from atmospheric air, thereby diminishing fuel consumption and reducing overall rocket launch costs. This project concentrates on crafting a three-dimensional . N° de réf. du vendeur 1405391131
Quantité disponible : Plus de 20 disponibles
Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne
Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -The ejector mode concept in rocket-based combined cycles presents an opportunity to derive thrust from atmospheric air, thereby diminishing fuel consumption and reducing overall rocket launch costs. This project concentrates on crafting a three-dimensional rocket nozzle featuring the ejector effect. The design involves a diverging section passing through a non-axisymmetric gate or clover on the outer perimeter, creating a void for air intake into the center of an annular rocket exhaust stream. The primary objective is to pinpoint the optimal design among three configurations with varying clover numbers (3, 4, and 5). Flow analyses, utilizing numerical simulations and a predefined Mach number distribution, were conducted, incorporating viscous simulations with the k-¿ turbulence model. Results reveal that the nozzle with 4 clovers outperforms those with 3 or 5 clovers, aligning closely with predefined outlet Mach numbers and demonstrating effectiveness.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 68 pp. Englisch. N° de réf. du vendeur 9786207460793
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Vendeur : preigu, Osnabrück, Allemagne
Taschenbuch. Etat : Neu. RBCC Rocket Nozzle: Modelling and Dynamic Analysis | Optimizing Thrust: A Rocket Nozzle Analysis Approach | Kalyan Charan A | Taschenbuch | Englisch | 2024 | LAP LAMBERT Academic Publishing | EAN 9786207460793 | Verantwortliche Person für die EU: SIA OmniScriptum Publishing, Brivibas Gatve 197, 1039 RIGA, LETTLAND, customerservice[at]vdm-vsg[dot]de | Anbieter: preigu. N° de réf. du vendeur 128606033
Quantité disponible : 5 disponible(s)
Vendeur : Mispah books, Redhill, SURRE, Royaume-Uni
paperback. Etat : New. NEW. SHIPS FROM MULTIPLE LOCATIONS. book. N° de réf. du vendeur ERICA82362074607906
Quantité disponible : 1 disponible(s)