By Gibbs G.W.
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A hundred and one PAGES fresh PLASTIC LAMINATION OVER PAPERJACKET
Dieses Buch wendet sich an Studenten der Ingenieurwissenschaften und Ingenieure der Raumfahrtindustrie und der Energieverfahrenstechnik. Es verkn? pft die klassischen Gebiete der Aerodynamik mit der Nichtgleichgewichts-Thermodynamik hei? er Gase. Am Beispiel des Wiedereintritts einer Raumkapsel in die Erdatmosph?
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Extra resources for Collected works. Thermodynamics
3 Variation of the ratio of the standard day static p r e s s u r e p to the sea level value PsL w i t h g e o m e t r i c altitude, Ref. 7 and App. B.
20. Once inside the engine, the air that has been compressed and burned would then require a nozzle exit area even larger than the original freestream capture area in order to make good on the available thrust, but a conventional nozzle of this geometry would be too cumbersome to carry along. Instead, the entire afterbody underneath the vehicle is used as a free expansion surface, Flight erbody Waves Airbreathing Engine Fig. 20 Schematic diagrams of aerospace plane flowtield and configuration. 26 H Y P E R S O N IAIRBREATHING C PROPULSION as depicted in Fig.
The reference configuration is called the S£nger Space Transportation System, in honor of the famous rocket and hypersonic flight pioneer Eugen S~nger, who first designed vehicles intended to fly to and from space. Hs'la6 As shown in Fig. 15, it is a reusable, two-stage, blended wing/body vehicle that employs horizontal takeoff and landing on conventional runways. The S£nger system emphasizes cost, safety, reliability, and flexibility, and uses advanced state-of-the-art technologies. The piloted first or lower stage has also been known as the European Hypersonic Transport Vehicle (EHTV) because it has wide commonality with a potential hypersonic passenger aircraft.