GrabCAD 模型信息
Supersonic tandem wing vs. single wing airplane · 模型 40281
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.
- 格式
- SOLIDWORKS、STL、STEP / IGES、Rendering、Other、Parasolid
- 分类
- Aerospace、Aviation、Speedrun
- 标签
- model、solid、solidworks、sldasm、sldprt、iges、igs、stl、biwedge、delta、bi-wedge、airfoil、diamond、simulation、flow、drone、jet、comparison、structural、aerodynamics、fea、cfd、tandem、flap、aileron、wing、mach、aircraft、supersonic、airplane
- 数据更新
- 2026-10-05T02:11:33Z
