One-Dimensional, Steady Flow with Mass Addition and the Effect of Combustion Chamber Flow on Rocket Thrust with a Supplement on the Integration of the Burning Equation-Reference-Cited by-同舟云学术

One-Dimensional, Steady Flow with Mass Addition and the Effect of Combustion Chamber Flow on Rocket Thrust with a Supplement on the Integration of the Burning Equation

Published:1955-02 Issue:2 Volume:25 Page:61-66
ISSN:1936-9980
Container-title:Journal of Jet Propulsion
language:en
Short-container-title:Journal of Jet Propulsion

Author:

PRICE E. W.¹

Affiliation:

1. U. S. Naval Ordnance Test Station, Inyokern, China Lake, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.6598

Reference10 articles.

1. The Mechanics and Thermodynamics of Steady One-Dimensional Gas Flow

2. Note on straight pipe jet motors

3. "Theory of Steady Flow with Mass Addition Applied to Solid Propellant Rocket Motors," by E. W. Price, Journal of the American Rocket Society, vol.23, July-August 1953.

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Stability of stationary subsonic compressible Euler flows with mass-additions in two-dimensional straight ducts;Journal of Differential Equations;2022-10

2. Numerical Study on Performance Effect of Burning-rate Ratio in Nozzleless Rocket Motor with Series Dual Burning Rate Grain;Journal of Energetic Materials;2021-01-22

3. Solid Rocket Enabling Technologies and Milestones in the United States;Journal of Propulsion and Power;2003-11

4. Internal Ballistics Considerations of Nozzleless Rocket Motors;Journal of Propulsion and Power;1999-11

5. Internal ballistics considerations of nozzleless rocket motors;31st Joint Propulsion Conference and Exhibit;1995-07-10