Reynolds Number Influence on Dual-Bell Transition Phenomena-Reference-Cited by-同舟云学术

Reynolds Number Influence on Dual-Bell Transition Phenomena

Published:2013-05 Issue:3 Volume:29 Page:602-609
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Verma S. B.¹,Stark R.²,Haidn O.²

Affiliation:

1. Experimental Aerodynamics Division, Council of Scientific and Industrial Research, National Aerospace Laboratories, 560 017 Bangalore, India

2. Institute of Space Propulsion, DLR, German Aerospace Center, 74219 Lampoldshausen, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34734

Reference30 articles.

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2. Advanced Rocket Nozzles

3. KasukaK.KumakawaA.NiinoM.KonnoA.AtsumiM. “Experimental Study on Extendible and Dual-Bell Nozzles Under High Altitude Conditions,” AIAA Paper 2002-3303, 2002.

4. FosterC.CowlesF. “Experimental Study of Gas-Flow Separation in Overexpanded Exhaust Nozzles for Rocket Motors,” Jet Propulsion Lab. California Inst. of Technology, Progress Rept. 4-103, 1949.

5. HornM.FisherS. “Dual-Bell Altitude Compensating Nozzle,” NASA CR-194719, 1994.

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