Intermittent Detonation as a Thrust-Producing Mechanism-Reference-Cited by-同舟云学术

Intermittent Detonation as a Thrust-Producing Mechanism

Published:1957-05 Issue:5 Volume:27 Page:534-541
ISSN:1936-9980
Container-title:Journal of Jet Propulsion
language:en
Short-container-title:Journal of Jet Propulsion

Author:

NICHOLLS J. A.¹,WILKINSON H. R.¹,MORRISON R. B.¹

Affiliation:

1. University of Michigan, Ann Arbor, Mich.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.12851

Reference16 articles.

1. Morrison, R. B. "A Shock Tube Investigation of Detonative Combustion," Report UMM-97, University of Michigan,Engineering Research Institute Project M898,Jan. 1952.

2. Bitondo, D., and Bollay, W. "Preliminary Performance Analysis of the Pulse-Detonation-Jet Engine System," Aerophysics Development Corp. Report ADC-102-1, April 1952.

Cited by 198 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. Influence of fuel inhomogeneity on detonation wave propagation in a rotating detonation combustor;Shock Waves;2024-08-30

2. On the Challenges of Integrating a Rotating Detonation Combustor With an Industrial Gas Turbine and Important Design Considerations for Row-1 Blades;Journal of Engineering for Gas Turbines and Power;2024-08-23

3. Primary investigation on Ram-Rotor Detonation Engine;Chinese Journal of Aeronautics;2024-05

4. Experimental demonstration on detonation initiation by laser ignition and shock focusing in elliptical cavity;Shock Waves;2023-12

5. Characteristics of rotating detonation wave fueled by liquid kerosene with increasing equivalence ratios;FirePhysChem;2023-12