Conceptual Design of Low-Boom Supersonic Aircraft with Flight Trim Requirement
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2141
Reference17 articles.
1. Optimization and Adjoint-Based CFD for the Conceptual Design of Low Sonic Boom Aircraft
2. Adjoint-based low-boom design with Cart3D (Invited)
3. Application of Adjoint Methodology to Supersonic Aircraft Design Using Reversed Equivalent Areas
4. Integration of Off-Track Sonic Boom Analysis for Supersonic Aircraft Conceptual Design
5. Generation of Parametric Equivalent-Area Targets for Design of Low-Boom Supersonic Concepts
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