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Showing 1 to 3 of 3 for “"shock-shock interaction"”.

  1. Experimental Investigation of Shock-Shock Interactions over a 2-D Wedge at M = 6

    … and sweep angle on peak heating rates due to shock-shock interactions were investigated in the NASA Langley Research Center 20-inch Mach 6 Air Tunnel. The fin model leading edges, which represent cylindrical leading edges or struts on hypersonic vehicles, were varied from 0.25 inches to 0.75 …

    vt Repository record for Experimental Investigation of Shock-Shock Interactions over a 2-D Wedge at M = 6 (opens in a new tab)

  2. Model Reduction of Computational Aerothermodynamics for Multi-Discipline Analysis in High Speed Flows

    … flows over deformed surfaces with shock-shock interaction and shock-boundary layer interaction. An additional focus of this dissertation is on the implementation and computation of results using the developed aerodynamic heating and pressure models in complex …

    ohiolink Repository record for Model Reduction of Computational Aerothermodynamics for Multi-Discipline Analysis in High Speed Flows (opens in a new tab)

  3. Improving the Performance of Re-entry Vehicle in Hypersonic Flow by Morphing Nose cone by Bio-Mimicking Honey Bee Abdomen

    … flat D-aerospike. The presence of a strong bow shock in honey bee abdomen morphed nosecone without spike generates significant drag, which diminishes in its alternate position. During the honey bee 's extension, both at 2.5 degrees and 5 degrees, the drag appears relatively minimal due to the …

    southwales Repository record for Improving the Performance of Re-entry Vehicle in Hypersonic Flow by Morphing Nose cone by Bio-Mimicking Honey Bee Abdomen (opens in a new tab)