Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2581
Reference49 articles.
1. Hybrid CART3D/OVERFLOW Near-Field Analysis of a Low Boom Configuration with Wind Tunnel Comparisons (Invited)
2. USM3D Analysis of Low Boom Configuration (Invited)
3. Low Boom Configuration Analysis with FUN3D Adjoint Simulation Framework (Invited)
4. Sonic Boom Computations for a Mach 1.6 Cruise Low Boom Configuration and Comparisons with Wind Tunnel Data (Invited)
5. Sonic-Boom Prediction of a Scaled Low-Boom Demonstration Aircraft Considering Viscosity Effects
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