Design-Oriented Aerodynamic Analysis for Supersonic Laminar Flow Wings.
類似資料:
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
9
テクニカルペーパー
A parametric study of supersonic laminar flow for swept wings using linear stability analysis
National Aeronautics and Space Adminstration |
4
テクニカルペーパー
Conceptual Design of Conventional and Oblique Wing Configurations for Small Supersonic Aircraft
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |