Unsteady Flow Conditions During Dual-Bell Sneak Transition-Reference-Cited by-同舟云学术

Unsteady Flow Conditions During Dual-Bell Sneak Transition

Published:2015-07 Issue:4 Volume:31 Page:1175-1183
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,Hadjadj A.²,Haidn O.³

Affiliation:

1. Flow Structure Management and Aircraft and Spacecraft Aerodynamics, Council of Scientific and Industrial Research–National Aerospace Laboratories, Bangalore 560017, India

2. Institut National des Sciences Appliquées de Rouen, 76801 St Etienne du Rouvray, France

3. Technische Universität München, 85748 Garching, 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.B35558

Reference24 articles.

1. 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, Pasadena, CA, 1949.

2. SuttonN. N. “Liquid Rocket Engine Nozzles,” NASA Space Vehicle Design Criteria, NASA SP-8120, 1976.

3. Advanced Rocket Nozzles

4. Critical Assessment of Dual-Bell Nozzles

5. Role of Wall Shape on the Transition in Axisymmetric Dual-Bell Nozzles

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