Aerodynamic and Inlet Flow Characteristics of Several Hypersonic Airbreathing Missile Concepts
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.57486
Reference8 articles.
1. Performance Potential and Research Needs of a Hypersonic, Airbreathing, Lifting Missile Concept
2. The integral-rocket, dual-combustion ramjet - A new propulsion concept
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3. Application of Taguchi Design Methods and Uniform Design Methods to Scramjet Propulsion System Optimization for Hypersonic Cruise Vehicle;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26
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