Design and performance evaluation of a dual bell nozzle-Reference-Cited by-同舟云学术

Design and performance evaluation of a dual bell nozzle

Published:2017-01 Issue: Volume:130 Page:52-59
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Kbab H.,Sellam M.,Hamitouche T.,Bergheul S.,Lagab L.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference17 articles.

1. Experimental study of gas flow separation in overexpanded exhaust nozzles for rocket motors (Progress report 4-103);Foster,1949

2. Dual-bell altitude compensating nozzles;Horn;Rocket. Div.,1994

3. Th. Alziary de Roquefort, P. Comte, S. Girard, A. Lebedev, A.-T. Nguyen, T.-H.-H. Le, Charges Latérales dans les Tuyères Axisymétriques, ATAC Technical Report.

4. Numerical analysis of the performance of altitude compensating dual bell nozzle flows;Goel;Rocket. Div.,1995

5. G. Hagemann, M. Frey, D. Manski, A critical assessment of dual-bell nozzles, in: Proceedings of the 33rd AIAA Joint Propulsion Conference, Seattle, WA, AIAA-97-3299, July 1997.

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