Deflagration-to-Detonation Transition in Nitrous Oxide/Oxygen-Fuel Mixtures for Propulsion-Reference-Cited by-同舟云学术

Deflagration-to-Detonation Transition in Nitrous Oxide/Oxygen-Fuel Mixtures for Propulsion

Published:2019-09 Issue:5 Volume:35 Page:944-952
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Bangalore Venkatesh Prashanth¹,Meyer Scott E.¹,Bane Sally P. M.¹,Grubelich Mark C.²

Affiliation:

1. Purdue University, West Lafayette, Indiana 47907

2. Sandia National Laboratories, Albuquerque, New Mexico 87185

Funder

Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.B37391

Reference54 articles.

1. TauschekM. J.CorringtonL. C.HuppertM. C. “Nitrous Oxide Supercharging of an Aircraft Engine Cylinder,” NACA Wartime Rept. E-199, Lewis Flight Propulsion Lab, Cleveland, OH, June 1945.

2. LaughreyJ. A.BollingerL. E.EdseR. “Detonability of Nitrous Oxide at Elevated Initial Temperature and Pressure,” ARL 62-432, Wright-Patterson Air Force Base, OH, 1962.

3. JostA.MichelK. W.TroeJ.WagnerH. G. “Detonation and Shock-Tube Studies of Hydrazine and Nitrous Oxide,” ARL 63-157, Wright-Patterson Air Force Base, OH, 1963.

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