Simulations and Experiments of a Dual-Stream Low-Boom Supersonic Inlet
Author:
Affiliation:
1. Turbine Aerodynamics Engineer, University of Virginia, Charlottesville, Virginia 22904
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35610
Reference21 articles.
1. Canonical Normal Shock Wave/Boundary-Layer Interaction Flows Relevant to External Compression Inlets
2. Supersonic Inlet Shaping for Dramatic Reductions in Drag and Sonic Boom Strength
3. Simulations of a low-boom, axisymmetric, external compression inlet
4. ChimaR. “Analysis of Buzz in a Supersonic Inlet,” NASA TM-2012-217612, 2012.
5. Coupled Analysis of an Inlet and Fan for a Quiet Supersonic Jet
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