Scram jet component optimization using CFD and design of experiments

Author:

Hagenmaier M.1,Davis D.

Affiliation:

1. USAF, Research Lab., Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. Vanderplaats Research and Development, Inc. "VisualDOC Getting Started Manual Version 2.0," (2001).

2. Computational Analysis for Rocket-Based Combined-Cycle Systems During Rocket-Only Operation

3. Multi-criteria design optimization of two-dimensional supersonic inlet

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2. Design and Optimization of a Notional Scramjet by Means of Stream Thrust Analysis and Design of Experiments;19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2014-06-13

3. Improved Simulation of Inflow Distortion for Direct-Connect Scramjet Combustor;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

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5. Experimental Investigation of Hydrocarbon-fuel Ignition in Scramjet Combustor;Chinese Journal of Aeronautics;2004-05

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