Minimum Trim Drag for a Three-Surface Supersonic Transport Aircraft
Author:
Affiliation:
1. University of Michigan
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3472
Reference31 articles.
1. The theoretical minimum induced drag of three-surface airplanes in trim
2. A General Approach to Multiple Lifting Surface Design and Analysis
3. Aerodynamic tradeoff study of conventional, canard, and trisurface aircraft systems
4. Three-surface aircraft - Optimum vs typical
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1. Tare & Interference Corrections for Commercial Supersonic Configurations Tested at the University of Washington’s Kirsten Wind Tunnel;AIAA SCITECH 2024 Forum;2024-01-04
2. Supersonic Configurations at Low Speeds (SCALOS): Progress at the University of Washington;AIAA SCITECH 2024 Forum;2024-01-04
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