System Performance and Thermodynamic Cycle Analysis of Airbreathing Pulse Detonation Engines-Reference-Cited by-同舟云学术

System Performance and Thermodynamic Cycle Analysis of Airbreathing Pulse Detonation Engines

Published:2003-07 Issue:4 Volume:19 Page:556-567
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Wu Yuhui¹,Ma Fuhua¹,Yang Vigor¹

Affiliation:

1. Pennsylvania State University, University Park, Pennsylvania 16802

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/10.2514/2.6166

Reference80 articles.

1. Configurations Isp, s and Thrust, N H2/O2, Sterling et al.7Single tube, f D 33 Hz, i.d. D 2:2 cm, L D 15: 2 cm N/A

2. atm, (1996) fully filled, H2and O2adopted as buffer gases, spark ignitor 298 K, Stuessy and Single tube, f D 10-12 Hz, fully filled, air used as buffer gas N/A Á D 1:0 Wilson21cylindrical tube with i.d. D 7:6 cm, L D 53:3 cm

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