Boundary-Layer Effects on Internal Flow Choking in Dual-Thrust Solid Rocket Motors-Reference-Cited by-同舟云学术

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Boundary-Layer Effects on Internal Flow Choking in Dual-Thrust Solid Rocket Motors

Published:2008-03 Issue:2 Volume:24 Page:224-235
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Kumar V. R. Sanal¹,Raghunandan B. N.²,Kawakami T.³,Kim H. D.⁴,Setoguchi T.⁵,Raghunathan S.⁶

Affiliation:

1. Vikram Sarabhai Space Centre, Trivandrum 695 022, Kerala, India

2. Indian Institute of Science, Bangalore 560 012, India

3. Hosei University, Tokyo 184-8584, Japan

4. Andong National University, Andong 760-749, Republic of Korea

5. Saga University, Saga 840-8502, Japan

6. Queen’s University of Belfast, Northern Ireland BT7 1NN, United Kingdom

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/10.2514/1.30649

Reference37 articles.

1. Starting Transient of Solid-Propellant ocket Motors with High Internal Gas Velocities

2. Starting Transient Flow Phenomena in Inert Simulators of Solid Rocket Motors with Divergent Ports

3. Studies on Internal Flow Choking in Dual-Thrust Motors

4. Fluid-Throat-Induced Shock Waves During the Ignition Transient of Solid Rockets

5. Flame Spread with Sudden Expansions of Ports of Solid Propellant Rockets

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3. Phenomenological Introduction of Standoff Distance of Sonic Ring Impelling Entropy Waves and Aerodynamic Heating of Hypersonic Vehicles;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27

4. Demonstration of Sanal Flow Choking and/or Streamtube Flow Choking in 3D Reacting Flows Causing Detonation and Explosions;AIAA SCITECH 2023 Forum;2023-01-19

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