Performance Assessment of a Large Scale Pulsejet-Driven Ejector System

Author:

Paxson Daniel1,Litke Paul2,Schauer Frederick2,Bradley Royce3,Hoke John3

Affiliation:

1. NASA Glenn Research Center

2. U.S. Air Force Research Laboratory

3. Innovative Scientific Solutions, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Cited by 12 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. Operational mechanism of valved-pulsejet engines;Aerospace Science and Technology;2024-05

2. CFD investigation of pulse jet engine using different combustion models;PROCEEDINGS OF THE 1ST INTERNATIONAL CONFERENCE ON FRONTIER OF DIGITAL TECHNOLOGY TOWARDS A SUSTAINABLE SOCIETY;2023

3. Modelling & numerical exploration of pulsejet engine using eddy dissipation combustion model;Materials Today: Proceedings;2020

4. Revisiting the Argus pulsejet engine of V-1 buzz bombs: An experimental investigation of the first mass-produced pressure gain combustion device;Experimental Thermal and Fluid Science;2019-12

5. Computational Study of Pulsejet-Driven Pressure Gain Combustors at High-Pressure;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12

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