This report describes three calibration models in the AGARD series. Model G: A slender wing. Suitable for tests over a wide speed range. Fitted with a fin and a sting fairing. Model H: A thin tapered wing suitable for high speed tests. Model J: A 10 degree semi-angle cone, suitable for high supersonic speed testing. (Author)
Calibration Models for Dynamic Stability Tests
1968
8 pages
Report
No indication
English
Aircraft , Fluid Mechanics , Delta wings , Aerodynamic characteristics , Slender bodies , Thin wings , Conical bodies , Wind tunnel models , Boundary layer transition , Calibration , Subsonic characteristics , Transonic characteristics , Supersonic characteristics , Standardization , Walls , Interference , Fins , Slender wings , Sting mounts , Calibration models
Calibration Models for Dynamic Stability Tests
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