Numerical Investigation of Flow Transition Behavior in Cold Flow Dual-Bell Rocket Nozzles-Reference-Cited by-同舟云学术

Numerical Investigation of Flow Transition Behavior in Cold Flow Dual-Bell Rocket Nozzles

Published:2016-09 Issue:5 Volume:32 Page:1212-1219
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Schneider Dirk¹,Génin Chloé¹

Affiliation:

1. DLR, German Aerospace Center, D-74239 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.B36010

Reference11 articles.

1. FosterC. R.CowlesF. B. “Experimental Study of Gas-Flow Separation in Overexpanded Exhaust Nozzles for Rocket Motors,” Jet Propulsion Lab. Technical Rept. JPL-PR-4-103, Pasadena, CA, 1949.

2. HornM.FisherS. “Dual-Bell Altitude Compensating Nozzles,” NASA CR-194719, 1994.

3. Experimental Study on Flow Transition in Dual Bell Nozzles

4. A one-equation turbulence model for aerodynamic flows

5. A flux splitting scheme with high-resolution and robustness for discontinuities

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