Supersonic Dual Bell Axisymmetric Minimum Length Nozzle Conception for High Propulsion Thrust

Author:

Zebbiche Toufik

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference29 articles.

1. Horn M, Fisher S (1994) Dual-bell altitude compensating nozzles, Rocketdyne Division. NASA CR-194719

2. Hagemann G, Immich H, Nguyen TV, Dumnov GE (1998) Advanced rocket nozzles. J Propul Power 14(5):620–634

3. Dumonov G, Ponomaryov NB, Voinov AL (1997) Dual-bell nozzles for rocket engines of launch vehicle upper stages and orbital transfer vehicles, AIAA Paper 97-3089, 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, USA, Jully 6–7

4. Goel P, Jensen R (1995) Numerical analysis of the performance of altitude compensating dual-bell nozzle flow, In: 7th annual symposium, Vol. II, NASA Marshall Space Flight Center, AL

5. Martelli E, Nasuti F, Onofri M (2007) Numerical parametric analysis of dual-bell nozzle flows. AIAA J 45(6):40–50

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