Numerical Investigation of Dual-Mode Operation in a Rectangular Scramjet Flowpath
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, Ohio State University, Columbus, Ohio 43210
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/10.2514/1.B34994
Reference51 articles.
1. Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment
2. The Hypersonic Collaborative Australia/United States Experiment (HyCAUSE)
3. Development of an In-Flight Non-Intrusive Mass Capture System
4. CabellK.HassN.StorchA.GruberM. “HIFiRE Direct-Connect Rig (HDCR) Phase I Scramjet Test Results from the NASA Langely Arc-Heated Scramjet Test Facility,” AIAA Paper 2011-2248, 2011.
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