Optimization of an engine-integrated waverider with steady state flight constraints
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1995-848
Reference23 articles.
1. Active Control of Aerothermoelastic Effects for a Conceptual Hypersonic Aircraft
2. 'O'Neill, M. K., Optimized Scramjet Engine Integration on a Waverider Airfrme. PhD thesis,University of Maryland, 1992.
3. Research and design for lifting reentry
4. 'Ferguson, F., Ezpanding the Waverider Design Space Using Arbitrary Generating Flowfields. PhD thesis,University of Maryland, 1993.
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