A waverider derived hypersonic X-vehicle
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1995-6162
Reference22 articles.
1. The effects of hypersonic flight test requirements on research vehicle design
2. A hypersonic waverider research vehicle
3. 3D CFD analysis of a SR71-waverider launch configuration
4. Januruy 1995;Haney J.W.
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1. Research on the drag reduction performance induced by the counterflowing jet for waverider with variable blunt radii;Acta Astronautica;2016-10
2. The Construction of Analytic Hypersonic Pitch Moment Coefficients Using a Curl Transformation;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
3. Bluntness impact on performance of waverider;Computers & Fluids;2011-09
4. Off-design regimes of flow past waveriders based on isentropic compression flows;Fluid Dynamics;2010-04
5. Numerical investigation of off-design regimes of flow past waveriders on the basis of axisymmetric conical flows;Fluid Dynamics;2007-04
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