Author:
Hadjadj Abdellah,Onofri Marcello
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Reference48 articles.
1. Lawrence, R.A.: Symmetrical and unsymmetrical flow separation in supersonic nozzles. Research Report Number 67-1, Southern Methodist University (1967)
2. Verma S.B.: Study of flow separation in truncated ideal contour nozzle. J. Propuls. Power 18, 1112–1121 (2002)
3. Nave, L.H., Coffey, G.A.: Sea-level side loads in high-area-ratio rocket engines. AIAA Paper 73-1284 (1973)
4. Nguyen A.T., Deniau H., Girard S., Alziary de Requefort T.: Unsteadiness of flow separation and end-effects regime in a thrust-optimized contour rocket nozzle. Flow Turbul. Combust. 71, 1–21 (2003)
5. Hagemann G., Frey M., Koschel W.: Appearance of restricted shock separation in rocket nozzles. J. Propuls. Power 18, 577–584 (2002)
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