Supersonic tandem wing vs. single wing airplane
grabcad
I made this for my own curiosity; i wanted to see how much drag a tandem wing can spare in supersonic flight (Mach 2) in comparison to a single (standard) wing design, and how much lift will be lost during landing on that account.Folders contain: - AoA0 - results of simulation made at v=686m/s, angle of attack = 0°; STP conditions - AoA1 - results of simulation made at v=686m/s, angle of attack = 1°; STP conditions - AoA12-v100 - results of simulation made at v=100m/s, angle of attack = 12°; STP conditions - AoA12-v100+flaps - results of simulation made at v=100m/s, angle of attack = 12°, flaps down; STP conditions- negative-space-wing (structural) - model of a simple structure idea for the front wing (flaps, actuators and their attachments not included)While i am continuing this project, i will probably not upload the progress here.
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