RBCC engine-airframe integration on an osculating cone waverider vehicle
Author:
Affiliation:
1. Maryland, Univ., College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3823
Reference23 articles.
1. Tarpley, C., The Optimization of Engine - Integrated Hypersonic Waveriders withSteady State Flight and Static Margin Constraints. PhD thesis,University ofMaryland,College Park,1995.
2. O'Neill, M. K. L., Optimized Scramjet Engine Integration on a Waverider Airframe. PhD thesis,University of Maryland, CollegePark, 1992.
3. Takashima, N., Optimization of Waverider - Based Hypersonic Vehicle Designs. PhD thesis,University of Maryland, College Park, 1997.
4. Sensitivity of hydrocarbon combustion modeling for hypersonic missile design
5. The Strutjet engine - The overlooked option for space launch
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