Design of a film cooled dual-bell nozzle-Reference-Cited by-同舟云学术

Design of a film cooled dual-bell nozzle

Published:2019-05 Issue: Volume:158 Page:342-350
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Stark Ralf,Génin Chloé,Mader Christian,Maier Dietmar,Schneider Dirk,Wohlhüter Michael

Funder

German Research Foundation

Deutsche Forschungsgemeinschaft

DFG

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference69 articles.

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3. Rocket engine nozzle concepts, progress in astronautics and aeronautics, liquid rocket thrust chambers: aspects of modeling;Hagemann;Analysis, and Design,2004

4. Nozzle, US Patent 2,583,726, in France;Chalom,1948

5. E. Fischer, Nozzle Construction, US Patent 3,352,495.

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